Elongation

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Санкт-Петербургский государственный электротехнический университет "ЛЭТИ"

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Электротехника

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Shackelford J.F.Material science and engineering handbook.2001.pdf

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Table 254. ELONGATION OF TOOL STEELS

		Elongation
Type	Condition	(%)


L2	Annealed	25
	Oil quenched from 855 •C and single tempered at:
	205 •C	5
	315 •C	10
	425 •C	12
	540 •C	15
	650 •C	25
L6	Annealed	25
	Oil quenched from 845 •C and single tempered at:
	315 •C	4
	425 •C	8
	540 •C	12
	650 •C	20
S1	Annealed	24
	Oil quenched from 930 •C and single tempered at:
	205 •C
	315 •C	4
	425 •C	5
	540 •C	9
	650 •C	12
S5	Annealed	25
	Oil quenched from 870 •C and single tempered at:
	205 •C	5
	315 •C	7
	425 •C	9
	540 •C	10
	650 •C	15
S7	Annealed	25
	Fan cooled from 940 •C and single tempered at:
	205 •C	7
	315 •C	9
	425 •C	10
	540 •C	10
	650 •C	14

Source: Data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, p241, (1984).

Table 255. ELONGATION OF DUCTILE IRONS

		Elongation
Specification Number	Grade or Class	(%)


ASTM A395-76
ASME SA395	60-40-18	18
ASTM A476-70(d);
SAE AMS5316	80-60-03	3
ASTM A536-72,
MIL-1-11466B(MR)	60-40-18	18
	65-45-12	12
	80-55-06	6
	100-70-03	3
	120-90-02	2
SAE J434c	D4018	18
	D4512	12
	D5506	6
	D7003	3
MlL-I-24137(Ships)	Class A	15
	Class B	7
	Class C	20

Source: data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, p169, (1984).

Table 256. ELONGATION OF MALLEABLE IRON CASTINGS

		Elongation
Specification Number	Grade or Class	(%)


Ferritic
ASTM A47, A338; ANSI G48.1;
FED QQ-I-666c	32510	10
	35018	18
ASTM A197		5
Pearlitic and Martensitic
ASTM A220; ANSI C48.2;
MIL-I-11444B	40010	10
	45008	8
	45006	6
	50005	5
	60004	4
	70003	3
	80002	2
	90001	1
Automotive
ASTM A602; SAE J158	M3210	10
	M4504(a)	4
	M5003(a)	3
	M5503(b)	3
	M7002(b)	2
	M8501(b)	1

(a)Air quenched and tempered

(b)Liquid quenched and tempered

Source: data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, p171, (1984).

Table 257. ELONGATION OF FERRITIC STAINLESS STEELS

(SHEET 1 OF 2)

				Elongation
Type	ASTM Specification	Form	Condition	(%)


Type 405 (UNS S40500)	A580	Wire	Annealed	20
	A580		Annealed, Cold Finished	16
Type 409 (UNS S40900)	—	Bar	Annealed	25(a)
Type 429 (UNS S42900)	—	Bar	Annealed	30(a)
Type 430 (UNS S43000)	A276	Bar	Annealed, Hot Finished	20
	A276		Annealed, Cold Finished	16
Type 430Ti(UNS S43036)	—	Bar	Annealed	30(a)
Type 434 (UNS S43400)	—	Wire	Annealed	33(a)
Type 436 (UNS S43600)	—	Sheet, Strip	Annealed	23(a)

(a) Typical Values

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p368 (1993).

Table 257. ELONGATION OF FERRITIC STAINLESS STEELS

(SHEET 2 OF 2)

				Elongation
Type	ASTM Specification	Form	Condition	(%)


Type 442 (UNS S44200)	—	Bar	Annealed	20(a)
Type 444 (UNS S44400)	A176	Plate, Sheet, Strip	Annealed	20
Type 446 (UNS S44600)	A276	Bar	Annealed, Hot Finished	20
	A276		Annealed, Cold Finished	16

(a) Typical Values

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p368 (1993).

Table 258. ELONGATION OF MARTENSITIC STAINLESS STEELS

(SHEET 1 OF 3)

				Elongation
Type	ASTM Specification	Form	Condition	(%)


Type 403 (UNS S40300)	A276	Bar	Annealed, hot ﬁnished	20
	A276		Annealed, cold ﬁnished	16
	A276		Intermediate temper, hot ﬁnished	15
	A276		Intermediate temper, cold ﬁnished	12
	A276		Hard temper, hot ﬁnished	12
	A276		Hard temper, cold ﬁnished	12
Type 410 (UNS S41000)	A276	Bar	Annealed, hot ﬁnished	20
	A276		Annealed, cold ﬁnished	16
	A276		Intermediate temper, hot ﬁnished	15
	A276		Intermediate temper, cold ﬁnished	12
	A276		Hard temper, hot ﬁnished	12
	A276		Hard temper, cold ﬁnished	12
Type 410S (UNS S41008)	A176	Plate, Sheet, Strip	Annealed	22
Type 410Cb (UNS S41040)	A276	Bar	Annealed, hot ﬁnished	13
	A276		Annealed, cold ﬁnished	12
	A276		Intermediate temper, hot ﬁnished	13
	A276		Intermediate temper, cold ﬁnished	12

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p369-370 (1993).

Table 258. ELONGATION OF MARTENSITIC STAINLESS STEELS

(SHEET 2 OF 3)

				Elongation
Type	ASTM Specification	Form	Condition	(%)


Type 414 (UNS S41400)	A276	Bar	Intermediate temper, hot ﬁnished	15
	A276		Intermediate temper, cold ﬁnished	15
Type 414L	—	Bar	Annealed	20
Type 420 (UNS S42000)	—	Bar	Tempered 205 °C	8
Type 422 (UNS S42200)	A565	Bar	Intermediate and hard tempers	13
Type 422 (UNS S42200)	A565	Bar	for high-temperature service	13
			for high-temperature service
Type 431 (UNS S43100)	—	Bar	Tempered 260 °C	16
	—		Tempered 595 °C	19
Type 440A (UNS S44002)	—	Bar	Annealed	20
	—		Tempered 315 °C	5
Type 440B (UNS S44003)	—	Bar	Annealed	18
	—		Tempered 315 °C	3
Type 440C (UNS S44004)	—	Bar	Annealed	14
	—		Tempered 315 °C	2

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p369-370 (1993).

Table 258. ELONGATION OF MARTENSITIC STAINLESS STEELS

(SHEET 3 OF 3)

				Elongation
Type	ASTM Specification	Form	Condition	(%)


Type 501 (UNS S50100)	—	Bar, Plate	Annealed	28
	—		Tempered 540 °C	15
Type 502 (UNS S50200)	—	Bar, Plate	Annealed	30

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p369-370 (1993).

Table 259. ELONGATION OF

PRECIPITATION -HARDENING AUSTENITIC STAINLESS STEELS

			Elongation
Type	Form	Condition	(%)


PH 13–8 Mo (UNS S13800)	Bar, Plate, Sheet, Strip	H950	6-10
		H1000	6-10
15–5 PH (UNS S15500) and 17–4 PH (UNS S17400)	Bar, Plate, Sheet, Stript	H900	10(a)
		H925	10(a)
		H1025	12(a)
		H1075	13(a)
		H1100	14(a)
		H1150	16(a)
		H1150M	18(a)
17–7 PH (UNS S17700)	Bar	RH950	6
		TH1050	6

(a) For ﬂat rolled products, value varies with thickness.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p371 (1993).

Table 260. ELONGATION OF HIGH–NITROGEN AUSTENITIC STAINLESS STEELS

	ASTM			Elongation
Type	Specification	Form	Condition	(%)


Type 201 (UNS S20100)	A276	Bar	Annealed	40
Type 202 (UNS S20200)	A276	Bar	Annealed	40
Type 205 (UNS S20500)	—	Plate	Annealed*	58
Type 304N (UNS S30451)	A276	Bar	Annealed	30
Type 304HN (UNS S30452)	—	Bar	Annealed	30
Type 316N (UNS S31651)	A276	Bar	Annealed	30

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p367 (1993).

*Typical values

Table 261. TOTAL ELONGATION OF

CAST ALUMINUM ALLOYS (SHEET 1 OF 3)

		Elongation (in 2 in.)
Alloy AA No.	Temper	(%)


201.0	T4	20
	T6	7
	T7	4.5
206.0, A206.0	T7	11.7
208.0	F	2.5
242.0	T21	1.0
	T571	0.5
	T77	2.0
	T571	1.0
	T61	0.5
295.0	T4	8.5
	T6	5.0
	T62	2.0
296.0	T4	9.0
	T6	5.0
	T7	4.5
308.0	F	2.0
319.0	F	2.0
	T6	2.0
	F	2.5
	T6	3.0
336.0	T551	0.5
	T65	0.5
354.0	T61	6.0
355.0	T51	1.5
	T6	3.0
	T61	1.0
	T7	0.5

Source: data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, (1984).

Table 261. TOTAL ELONGATION OF

CAST ALUMINUM ALLOYS (SHEET 2 OF 3)

		Elongation (in 2 in.)
Alloy AA No.	Temper	(%)


355.0 (Con’t)	T71	1.5
	T51	2.0
	T6	4.0
	T62	1.5
	T7	2.0
	T71	3.0
356.0	T51	2.0
	T6	3.5
	T7	2.0
	T71	3.5
	T6	5.0
	T7	6.0
357.0, A357.0	T62	8.0
359.0	T61	6.0
	T62	5.5
360.0	F	3.0
A360.0	F	5.0
380.0	F	3.0
383.0	F	3.5
384.0, A384.0	F	2.5
390.0	F	1.0
	T5	1.0
A390.0	F,T5	<1.0
	T6	<1.0
	T7	<1.0
	F,T5	1.0
	T6	<1.0
	T7	<1.0

Source: data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, (1984).

Table 261. TOTAL ELONGATION OF

CAST ALUMINUM ALLOYS (SHEET 3 OF 3)

		Elongation (in 2 in.)
Alloy AA No.	Temper	(%)


413.0	F	2.5
A413.0	F	3.5
443.0	F	8.0
B443.0	F	10.0
C443.0	F	9.0
514.0	F	9.0
518.0	F	5.0—8.0
520.0	T4	16
535.0	F	13
712.0	F	5.0
713.0	T5	3.0
	T5	4.0
771.0	T6	9.0
850.0	T5	10.0

Source: data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, (1984).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 1 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C10100 Oxygen-free electronic	99.99 Cu	F, R, W, T, P, S	55(4)
C10200 Oxygen-free copper	99.95 Cu	F, R, W, T, P, S	55(4)
C10300 Oxygen-free extra-low phosporus	99.95 Cu, 0.003 P	F, R, T, P, S	50(6)
C10400, C10500, C10700 Oxygen-free, silver-bearing	99.95 Cu(e)	F, R, W, S	55(4)
C10800 Oxygen-free, low phosporus	99.95 Cu, 0.009 P	F, R, T, P	50(4)
CS11000 Electrolytic tough pitch copper	99.90 Cu, 0.04 O	F, R, W, T, P, S	55(4)
C11100 Electrolytic tough pitch, anneal resistant	99.90 Cu, 0.04 O, 0.01 Cd	W	(60)
C11300, C11400, C11500, C11600 Silver-bearing tough pitch copper	99.90 Cu, 0.04 O, Ag(f)	F, R, W, T, S	55(4)
C12000, C12100	99.9 Cu(g)	F, T, P	55(4)
C12200 Phosphorus deoxidized copper, high residual phosphorus	99.90 Cu, 0.02 P	F, R, T, P	45(8)
C12500, C12700, C12800, C12900, C13000 Fire-reﬁned tough pitch with silver	99.88 Cu(h)	F, R, W, S	55(4)
C14200 Phosphorus deoxidized, arsenical	99.68 Cu, 0.3 As, 0.02 P	F, R, T	45(8)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 2 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C19200	98.97 Cu, 1.0 Fe, 0.03 P	F, T	40
C14300	99.9 Cu, 0.1 Cd	F	42(l)
C14310	99.8 Cu, 0.2 Cd	F	42(l)
C14500 Phosphorus deoxidized, tellurium bearing	99.5 Cu, 0.50 Te, 0.008 P	F, R, W, T	50(3)
C14700 Sulfur bearing	99.6 Cu, 0.40 S	R, W	52(8)
C15000 Zirconium copper	99.8 Cu, 0.15 Zr	R, W	54(1.5)
C15500	99.75 Cu, 0.06 P, 0.11 Mg, Ag(i)	F	40(3)
C15710	99.8 Cu, 0.2 Al2O3	R, W	20(10)
C15720	99.6 Cu, 0.4 Al2O3	F, R	20(3.5)
C15735	99.3 Cu, 0.7 Al2O3	R	16(10)
C15760	98.9 Cu, 1.1 Al2O3	F, R	20(8)
C16200 Cadmium copper	99.0 Cu, 1.0 Cd	F, R, W	57(1)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 3 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C16500	98.6 Cu, 0.8 Cd, 0.6 Sn	F, R, W	53(1.5)
C17000 Beryllium copper	99.5 Cu, 1.7 Be, 0.20 Co	F, R	45(3)
C17200 Beryllium copper	99.5 Cu, 1.9 Be , 0.20 Co	F, R, W, T, P, S	48(1)
C17300 Beryllium copper	99.5 Cu, 1.9 Be, 0.40 Pb	R	48(3)
C17500 Copper-cobalt-beryllium alloy	99.5 Cu, 2.5 Co, 0.6 Be	F, R	28(5)
C18200, C18400, C18500 Chromium copper	99.5 Cu(j)	F, W, R, S, T	40(5)
C18700 leaded copper	99.0 Cu, 1.0 Pb	R	45(8)
C18900	98.75 Cu, 0.75 Sn, 0.3 Si, 0.20 Mn	R, W	48(14)
C19000 Copper-nickel-phosphorus alloy	98.7 Cu, 1.1 Ni, 0.25 P	F, R, W	50
C19100 Copper-nickel-phosphorus-tellurium alloy	98.15 Cu, 1.1 Ni, 0.50 Te, 0.25 P	R, F	27(6)
C19400	97.5 Cu, 2.4 Fe, 0.13 Zn, 0.03 P	F	32

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 4 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C19500	97.0 Cu, 1.5 Fe, 0.6 Sn, 0.10 P, 0.80 Co	F	15
C21000 Gilding, 95%	95.0 Cu, 5.0 Zn	F, W	45(4)
C22000 Commercial bronze, 90%	90.0 Cu, 10.0 Zn	F, R, W, T	50(3)
C22600 Jewelry bronze, 87.5%	87.5 Cu, 12.5 Zn	F, W	46(3)
C23000 Red brass, 85%	85.0 Cu, 15.0 Zn	F, W, T, P	55(3)
C24000 Low brass, 80%	80.0 Cu, 20.0 Zn	F, W	55(3)
C26000 Cartridge brass, 70%	70.0 Cu, 30.0 Zn	F, R, W, T	66(3)
C26800, C27000 Yellow brass	65.0 Cu, 35.0 Zn	F, R, W	65(3)
C28000 Muntz metal	60.0 Cu, 40.0 Zn	F, R, T	52(10)
C31400 Leaded commercial bronze	89.0 Cu, 1.75 Pb, 9.25 Zn	F, R	45(10)
C31600 Leaded commercial bronze, nickel-bearing	89.0 Cu, 1.9 Pb, 1.0 Ni, 8.1 Zn	F, R	45(12)
C33000 Low-leaded brass tube	66.0 Cu, 0.5 Pb, 33.5 Zn	T	60(7)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 5 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C33200 High-leaded brass tube	66.0 Cu, 1.6 Pb, 32.4 Zn	T	50(7)
C33500 Low-leaded brass	65.0 Cu, 0.5 Pb, 34.5 Zn	F	65(8)
C34000 Medium-leaded brass	65.0 Cu, 1.0 Pb, 34.0 Zn	F, R, W, S	60(7)
C34200 High-leaded brass	64.5 Cu, 2.0 Pb, 33.5 Zn	F, R	52(5)
C34900	62.2 Cu, 0.35 Pb, 37.45 Zn	R, W	72(18)
C35000 Medium-leaded brass	62.5 Cu, 1.1 Pb, 36.4 Zn	F, R	66(1)
C35300 High-leaded brass	62.0 Cu, 1.8 Pb, 36.2 Zn	F, R	52(5)
C35600 Extra-high-leaded brass	63.0 Cu, 2.5 Pb, 34.5 Zn	F	50(7)
C36000 Free-cutting brass	61.5 Cu, 3.0 Pb, 35.5 Zn	F, R, S	53(18)
C36500 to C36800 Leaded Muntz metal	60.0 Cu(k), 0.6 Pb, 39.4 Zn	F	45
C37000 Free-cutting Muntz metal	60.0 Cu, 1.0 Pb, 39.0 Zn	T	40(6)
C37700 Forging brass	59.0 Cu, 2.0 Pb, 39.0 Zn	R, S	45

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 6 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C38500 Architectural bronze	57.0 Cu, 3.0 Pb, 40.0 Zn	R, S	30
C40500	95 Cu, 1 Sn, 4 Zn	F	49(3)
C40800	95 Cu, 2 Sn, 3 Zn	F	43(3)
C41100	91 Cu, 0.5 Sn, 8.5 Zn	F, W	13
C41300	90.0 Cu, 1.0 Sn, 9.0 Zn	F, R, W	45
C41500	91 Cu, 1.8 Sn, 7.2 Zn	F	44
C42200	87.5 Cu, 1.1 Sn, 11.4 Zn	F	46
C42500	88.5 Cu, 2.0 Sn, 9.5 Zn	F	49
C43000	87.0 Cu, 2.2 Sn, 10.8 Zn	F	55(3)
C43400	85.0 Cu, 0.7 Sn, 14.3 Zn	F	49(3)
C43500	81.0 Cu, 0.9 Sn, 18.1 Zn	F, T	46(7)
C44300, C44400, C44500 Inhibited admiralty	71.0 Cu, 28.0 Zn, 1.0 Sn	F, W, T	65(0)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 7 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C46400 to C46700 Naval brass	60.0 Cu, 39.25 Zn, 0.75 Sn	F, R, T, S	50(17)
C48200 Naval brass, medium-leaded	60.5 Cu, 0.7 Pb, 0.8 Sn, 38.0 Zn	F, R, S	43(15)
C48500 Leaded naval brass	60.0 Cu, 1.75 Pb, 37.5 Zn, 0.75 Sn	F, R, S	40(15)
C50500 Phosphor bronze, 1.25% E	98.75 Cu, 1.25 Sn, trace P	F, W	48(4)
C51000 Phosphor bronze, 5% A	95.0 Cu, 5.0 Sn, trace P	F, R, W, T	64
C51100	95.6 Cu, 4.2 Sn, 0.2 P	F	48
C52100 Phosphor bronze, 8% C	92.0 Cu, 8.0 Sn, trace P	F, R, W	70
C52400 Phosphor bronze, 10% D	90.0 Cu, 10.0 Sn, trace P	F, R, W	70(3)
C54400 Free-cutting phosphor bronze	88.0 Cu, 4.0 Pb, 4.0 Zn, 4.0 Sn	F, R	50(15)
C60800 Aluminum bronze, 5%	95.0 Cu, 5.0 Al	T	55
C61000	92.0 Cu, 8.0 Al	R, W	65(25)
C61300	92.65 Cu, 0.35 Sn, 7.0 Al	F, R, T, P, S	42(35)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 8 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C61400 Aluminum bronze, D	91.0 Cu, 7.0 Al, 2.0 Fe	F, R, W, T, P, S	45(32)
C61500	90.0 Cu, 8.0 Al, 2.0 Ni	F	55(1)
C61800	89.0 Cu, 1.0 Fe, 10.0 Al	R	28(23)
C61900	86.5 Cu, 4.0 Fe, 9.5 Al	F	30(1)
C62300	87.0 Cu, 10.0 Al, 3.0 Fe	F, R	35(22)
C62400	86.0 Cu, 3.0 Fe, 11.0 Al	F, R	18(14)
C62500	82.7 Cu, 4.3 Fe, 13.0 Al	F, R	1
C63000	82.0 Cu, 3.0 Fe, 10.0 Al, 5.0 Ni	F, R	20(15)
C63200	82.0 Cu, 4.0 Fe, 9.0 Al, 5.0 Ni	F, R	25(20)
C63600	95.5 Cu, 3.5 Al, 1.0 Si	R, W	64(29)
C63800	99.5 Cu, 2.8 Al, 1.8 Si, 0.40 Co	F	36(4)
C64200	91.2 Cu, 7.0 Al	F, R	32(22)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 9 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C65100 Low-silicon bronze, B	98.5 Cu, 1.5 Si	R, W, T	55(11)
C65500 High-silicon bronze, A	97.0 Cu, 3.0 Si	F, R, W, T	63(3)
C66700 Manganese brass	70.0 Cu, 28.8 Zn, 1.2 Mn	F, W	60
C67400	58.5 Cu, 36.5 Zn, 1.2 Al, 2.8 Mn, 1.0 Sn	F, R	28(20)
C67500 Manganese bronze, A	58.5 Cu, 1.4 Fe, 39.0 Zn, 1.0 Sn, 0.1 Mn	R, S	33(19)
C68700 Aluninum brass, arsenical	77.5 Cu, 20.5 Zn, 2.0 Al, 0.1 As	T	55
C68800	73.5 Cu, 22.7 Zn, 3.4 Al, 0.40 Co	F	36
C69000	73.3 Cu, 3.4 Al, 0.6 Ni, 22.7 Zn	F	40
C69400 Silicon red brass	81.5 Cu, 14.5 Zn, 4.0 Si	R	25(20)
C70400	92.4 Cu, 1.5 Fe, 5.5 Ni, 0.6 Mn	F, T	46
C70600 Copper nickel, 10%	88.7 Cu, 1.3 Fe, 10.0 Ni	F, T	42(10)
C71000 Copper nickel, 20%	79.00 Cu, 21.0 Ni	F, W, T	40(3)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 10 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C71500 Copper nickel, 30%	70.0 Cu, 30.0 Ni	F, R, T	45(15)
C71700	67.8 Cu, 0.7 Fe, 31.0 Ni, 0.5 Be	F, R, W	40(4)
C72500	88.20 Cu, 9.5 Ni, 2.3 Sn	F, R, W, T	35(1)
C73500	72.0 Cu, 18.0 Ni , 10.0 Zn	F, R, W, T	37(1)
C74500 Nickel silver, 65-10	65.0 Cu, 25.0 Zn, 10.0 Ni	F, W	50(1)
C75200 Nickel silver, 65-18	65.0 Cu, 17.0 Zn, 18.0 Ni	F, R, W	45(3)
C75400 Nickel silver, 65-15	65.0 Cu, 20.0 Zn, 15.0 Ni	F	43
C75700 Nickel silver, 65-12	65.0 Cu, 23.0 Zn, 12.0 Ni	F, W	48

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

Table 262. ELONGATION OF WROUGHT COPPERS AND COPPER ALLOYS

(SHEET 11 OF 11)

			Elongation
	Nominal	Commercial	in 2 In
UNS Number and Name	Composition (%)	Forms(a)	(%)


C76200	59.0 Cu, 29.0 Zn, 12.0 Ni	F, T	50(1)
C77000 Nickel silver, 55-18	55.0 Cu, 27.0 Zn, 18.0 Ni	F, R, W	40
C72200	82.0 Cu, 16.0 Ni, 0.5 Cr, 0.8 Fe, 0.5 Mn	F, T	46(6)
C78200 Leaded nickel silver, 65-8-2	65.0 Cu, 2.0 Pb, 25.0 Zn, 8.0 Ni	F	40(3)

(a) F, ﬂat products; R, rod; W, wire; T, tube; P, pipe; S, shapes.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p442–454, (1993).

(d)Based on 100% for C360000.

(e)C10400, 8 oz/ton Ag; C10500, 10 oz/ton; C10700, 25 oz/ton .

(f)C11300, 8 oz/ton Ag; C11400,10 oz/ton; C11500, 16 oz/ton; C11600, 25 oz/ton

(g)C12000, 0.008 P; C12100, 0.008 P and 4 oz/ton Ag;

(h)C12700, 8 oz/ton Ag; C12800,10 oz/ton; C12900,16 oz/ton; C13000, 25 oz/ton.

(i)8.30 oz/ton Ag.

(j)C18200, 0.9 Cr; C18400, 0.8 Cr; C18500, 0.7 Cr

(k)Rod, 61.0 Cu min.

Table 263. ELONGATION OF COMMERCIALLY PURE TIN

Temperature	Elongation in 25mm
(°C)	(%)


Strained at 0.2 mm/m • min
-200	6
-160	15
-120	60
-80	89
-40	86
0	64
23	57
Strained at 0.4 mm/m • min
15	75
50	85
100	55
150	55
200	45

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p488, (1993).

Table 264. ELONGATION OF

COBALT-BASE SUPERALLOYS

	Temperature	Elongation
Alloy	(°C)	(%)


Haynes 25 (L–605) sheet	21	64
	540	59
	650	35
	760	12
	870	30
Haynes 188, sheet	21	56
	540	70
	650	61
	760	43
	870	73
S-816, bar	21	30
	540	27
	650	25
	760	21
	870	16

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p387, (1993).

Table 265. ELONGATION OF

NICKEL-BASE SUPERALLOYS (SHEET 1 OF 5)

	Temperature	Elongation
Alloy	(°C)	(%)


Astroloy, bar	21	16
	540	16
	650	18
	760	21
	870	25
D–979, bar	21	15
	540	15
	650	21
	760	17
	870	18
Hastelloy X, sheet	21	43
	540	45
	650	37
	760	37
	870	50
IN–102, bar	21	47
	540	48
	650	64
	760	110
	870	110
Inconel 600, bar	21	47
	540	47
	650	39
	760	46
	870	80
Inconel 601, sheet	21	45
	540	38
	650	45
	760	73
	870	92

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p387-389, (1993).

Table 265. ELONGATION OF

NICKEL-BASE SUPERALLOYS (SHEET 2 OF 5)

	Temperature	Elongation
Alloy	(°C)	(%)


Inconel 625, bar	21	50
	540	50
	650	35
	760	42
	870	125
Inconel 706, bar	21	19
	540	19
	650	21
	760	32
Inconel 718, bar	21	21
	540	18
	650	19
	760	25
	870	88
Inconel 718, sheet	21	22
	540	26
	650	15
	760	8
Inconel X-750, bar	21	24
	540	22
	650	9
	760	9
	870	47
M-252, bar	21	16
	540	15
	650	11
	760	10
	870	18

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p387-389, (1993).

Table 265. ELONGATION OF

NICKEL-BASE SUPERALLOYS (SHEET 3 OF 5)

	Temperature	Elongation
Alloy	(°C)	(%)


Nimonic 75, bar	21	41
	540	41
	650	42
	760	70
	870	68
Nimonic 80A, bar	21	24
	540	24
	650	18
	760	20
	870	34
Nimonic 90, bar	21	23
	540	23
	650	20
	760	10
	870	16
Nimonic 105, bar	21	12
	540	18
	650	24
	760	22
	870	25
Nimonic 115, bar	21	25
	540	26
	650	25
	760	22
	870	18
Pyromet 860, bar	21	22
	540	15
	650	17
	760	18

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p387-389, (1993).

Table 265. ELONGATION OF

NICKEL-BASE SUPERALLOYS (SHEET 4 OF 5)

	Temperature	Elongation
Alloy	(°C)	(%)


René 41, bar	21	14
	540	14
	650	14
	760	11
	870	19
René 95, bar	21	15
	540	12
	650	14
	760	15
Udimet 500, bar	21	32
	540	28
	650	28
	760	39
	870	20
Udimet 520, bar	21	21
	540	20
	650	17
	760	15
	870	20
Udimet 700, bar	21	17
	540	16
	650	16
	760	20
	870	27
Udimet 710, bar	21	7
	540	10
	650	15
	760	25
	870	29

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p387-389, (1993).

Table 265. ELONGATION OF

NICKEL-BASE SUPERALLOYS (SHEET 5 OF 5)

	Temperature	Elongation
Alloy	(°C)	(%)


Unitemp AF2–1DA, bar	21	10
	540	13
	650	13
	760	8
	870	8
Waspaloy, bar	21	25
	540	23
	650	34
	760	28
	870	35

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p387-389, (1993).

Table 266. DUCTILITY OF REFRACTORY METAL ALLOYS

(SHEET 1 OF 3)

					Low
		Alloying Additions			Temperature
Class	Alloy	(%)	Form	Condition	Ductility*


Niobium and Niobium	Pure Niobium	—	All	Recrystallized	A
Alloys	Pure Niobium	—	All	Recrystallized	A
Alloys
	Nb–1Zr	1 Zr	All	Recrystallized	A
	C103(KbI–3)	10 Hf, 1 Ti 0.7 Zr	All	Recrystallized	A
	SCb291	10 Ta, 10 W	Bar, Sheet	Recrystallized	A
	C129	10 W, 10 Hf, 0.1 Y	Sheet	Recrystallized	A
	FS85	28 Ta, 11 W, 0.8 Zr	Sheet	Recrystallized	A
	SU31	17 W, 3.5 Hf, 0.12 C, 0.03 Si	Bar, Sheet	Special Thermal Processing	C
Molybdenum and	Pure Molybdenum	—	All	Stress-relieved Annealed	B–C
Molybdenum Alloys	Pure Molybdenum	—	All	Stress-relieved Annealed	B–C
Molybdenum Alloys
	Doped Mo	K, Si; ppm levels	Wire, Sheet	Cold Worked	B
	Low C Mo	None	All	Stress-relieved Annealed	B
	TZM	0.5 Ti, 0.08 Zr, 0.015 C	All	Stress-relieved Annealed	B–C

* A excellent cryogenic ductility;

B excellent room-temperature ductility;

C may have marginal ductility at room temperature; D normally brittle at room temperature.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p390, (1993).

Table 266. DUCTILITY OF REFRACTORY METAL ALLOYS

(SHEET 2 OF 3)

					Low
		Alloying Additions			Temperature
Class	Alloy	(%)	Form	Condition	Ductility*


	TZC	1.0 Ti, 0.14 Zr, 0.02 to 0.08 C	All	Stress-relieved Annealed	B–C
	Mo–5Re	5 Re	All	Stress-relieved Annealed	B
	Mo–30W	30 W	All	Stress-relieved Annealed	B–C
Tantalum Alloys	Unalloyed	None	All	Recrystallized	A
	FS61	7.5 W(P/M)	Wire, Sheet	Cold Worked	A
	FS63	2.5 W, 0.15 Nb	All	Recrystallized	A
	TA–10W	10 W	All	Recrystallized	A
	KBI–40	40 Nb	All	Recrystallized	A
Tungsten Alloys	Unalloyed	None	Bar, Sheet,	Stress-relieved Annealed	D
Tungsten Alloys	Unalloyed	None	Wire	Stress-relieved Annealed	D
			Wire
	Doped	K, Si, Al; ppm levels	Wire	Cold Worked	C

* A excellent cryogenic ductility;

B excellent room-temperature ductility;

C may have marginal ductility at room temperature; D normally brittle at room temperature.

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p390, (1993).

Table 266. DUCTILITY OF REFRACTORY METAL ALLOYS

(SHEET 3 OF 3)

					Low
		Alloying Additions			Temperature
Class	Alloy	(%)	Form	Condition	Ductility*


	W–1 ThO2	1ThO2	Bar, Sheet,	Stress-relieved Annealed	D
	W–1 ThO2	1ThO2	Wire	Stress-relieved Annealed	D
	W–2 ThO2	2 ThO2	Bar, Sheet,	Stress-relieved Annealed	D
	W–2 ThO2	2 ThO2	Wire	Stress-relieved Annealed	D
	W–3 ThO2	3 ThO2	Bar, Wire	Stress-relieved Annealed	D
	W–4 ThO2	4 ThO2	Bar	Stress-relieved Annealed	D
	W–15 Mo	15 Mo	Bar, Wire	Stress-relieved Annealed	D
	W–50 Mo	50 Mo	Bar, Wire	Stress-relieved Annealed	D
	W–3 Re	3 Re	Wire	Cold Worked	C
	W–25 Re	25 Re	Bar, Sheet,	Stress-relieved Annealed	B
	W–25 Re	25 Re	Wire	Stress-relieved Annealed	B
			Wire


* A excellent cryogenic ductility;
B excellent room-temperature ductility;
C may have marginal ductility at room temperature;
D normally brittle at room temperature.
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p390, (1993).

Table 267. ELONGATION OF WROUGHT TITANIUM ALLOYS

AT ROOM TEMPERATURE (SHEET 1 OF 3)

			Elongation
Class	Alloy	Condition	(%)


Commercially Pure	99.5 Ti	Annealed	30
	99.2 Ti	Annealed	28
	99.1 Ti	Annealed	25
	99.0 Ti	Annealed	20
	99.2Ti-0.2Pd	Annealed	28
	Ti-0.8Ni-0.3Mo	Annealed	25
Alpha Alloys	Ti-5Al-2.5Sn	Annealed	16
	Ti-5Al-2.5Sn (low O2)	Annealed	16
Near Alpha Alloys	Ti-8Al-1Mo-1V	Duplex Annealed	15
	Ti-11Sn-1Mo-2.25Al-5.0Zr-1Mo-0.2Si	Duplex Annealed	15
	Ti-6Al-2Sn-4Zr-2Mo	Duplex Annealed	15
	Ti-5Al-2Sn-2Zr-2Mo-0.25Si	975 ˚C (1/2h), AC + 595 ˚C (2h), AC	13

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p512, (1993).

Table 267. ELONGATION OF WROUGHT TITANIUM ALLOYS

AT ROOM TEMPERATURE (SHEET 2 OF 3)

			Elongation
Class	Alloy	Condition	(%)


	Ti-6Al-2Nb-1Ta-1Mo	As rolled 2.5 cm (1 in.) plate	13
	Ti-6Al-2Sn-1.5Zr-1Mo- 0.35Bi-0.1Si	Beta forge + duplex anneal	11
Alpha-Beta Alloys	Ti-8Mn	Annealed	15
	Ti-3Al-2.5V	Annealed	20
	Ti-6Al-4V	Annealed	14
		Solution + age	10
	Ti-6Al-4V(low O2)	Annealed	15
	Ti-6Al-6V-2Sn	Annealed	14
		Solution + age	10
	Ti-7Al-4Mo	Solution + age	16
	Ti-6Al-2Sn-4Zr-6Mo	Solution + age	10
	Ti-6Al-2Sn-2Zr-2Mo- 2Cr-0.25Si	Solution + age	11
	Ti-10V-2Fe-3Al	Solution + age	10

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p512, (1993).

Table 267. ELONGATION OF WROUGHT TITANIUM ALLOYS

AT ROOM TEMPERATURE (SHEET 3 OF 3)

			Elongation
Class	Alloy	Condition	(%)


Beta Alloys	Ti-13V-1Cr-3Al	Solution + age	8
	Ti-8Mo-8V-2Fe-3Al	Solution + age	8
	Ti-3Al-8V-6Cr-4Mo-4Zr	Solution + age	7
		Annealed	15
	Ti-11.5Mo-6Zr-4.5Sn	Solution + age	11

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p512, (1993).

Table 268. ELONGATION OF WROUGHT TITANIUM ALLOYS

AT HIGH TEMPERATURE (SHEET 1 OF 4)

			Test
			Temperature	Elongation
Class	Alloy	Condition	(°C)	(%)


Commercially Pure	99.5 Ti	Annealed	315	32
	99.2 Ti	Annealed	315	35
	99.1 Ti	Annealed	315	34
	99.0 Ti	Annealed	315	25
	99.2Ti-0.2Pd	Annealed	315	37
	Ti-0.8Ni-0.3Mo	Annealed	205	37
	Ti-0.8Ni-0.3Mo	Annealed	315	32
Alpha Alloys	Ti-5Al-2.5Sn	Annealed	315	18
	Ti-5Al-2.5Sn (low O2)	Annealed	-195	16
			-255	15
Near Alpha Alloys	Ti-8Al-1Mo-1V	Duplex Annealed	315	20
			425	20
			540	25

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p512, (1993).

Table 268. ELONGATION OF WROUGHT TITANIUM ALLOYS

AT HIGH TEMPERATURE (SHEET 2 OF 4)

			Test
			Temperature	Elongation
Class	Alloy	Condition	(°C)	(%)


	Ti-11Sn-1Mo-2.25Al-5.0Zr-1Mo-0.2Si	Duplex Annealed	315	20
			425	22
			540	24
	Ti-6Al-2Sn-4Zr-2Mo	Duplex Annealed	315	16
			425	21
			540	26
	Ti-5Al-2Sn-2Zr-2Mo-0.25Si	975 ˚C (1/2h), AC + 595 ˚C (2h), AC	315	15
			425	17
			540	19
	Ti-6Al-2Nb-1Ta-1Mo	As rolled 2.5 cm (1 in.) plate	315	20
			425	20
			540	20
	Ti-6Al-2Sn-1.5Zr-1Mo- 0.35Bi-0.1Si	Beta forge + duplex anneal	480	15

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p512, (1993).

Table 268. ELONGATION OF WROUGHT TITANIUM ALLOYS

AT HIGH TEMPERATURE (SHEET 3 OF 4)

			Test
			Temperature	Elongation
Class	Alloy	Condition	(°C)	(%)


Alpha-Beta Alloys	Ti-8Mn	Annealed	315	18
	Ti-3Al-2.5V	Annealed	315	25
	Ti-6Al-4V	Annealed	315	14
		Annealed	425	18
		Annealed	540	35
		Solution + age	315	10
		Solution + age	425	12
		Solution + age	540	22
	Ti-6Al-4V(low O2)	Annealed	160	14
	Ti-6Al-6V-2Sn	Annealed	315	18
		Solution + age	315	12
	Ti-7Al-4Mo	Solution + age	315	18
			425	20

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p512, (1993).

Table 268. ELONGATION OF WROUGHT TITANIUM ALLOYS

AT HIGH TEMPERATURE (SHEET 4 OF 4)

			Test
			Temperature	Elongation
Class	Alloy	Condition	(°C)	(%)


	Ti-6Al-2Sn-4Zr-6Mo	Solution + age	315	18
			425	19
			540	19
	Ti-6Al-2Sn-2Zr-2Mo- 2Cr-0.25Si	Solution + age	315	14
	Ti-10V-2Fe-3Al	Solution + age	205	13
			315	13
Beta Alloys	Ti-13V-1Cr-3Al	Solution + age	315	19
			425	12
	Ti-8Mo-8V-2Fe-3Al	Solution + age	315	15
	Ti-3Al-8V-6Cr-4Mo-4Zr	Solution + age	315	20
			425	17
		Annealed	315	22
	Ti-11.5Mo-6Zr-4.5Sn	Solution + age	315	16

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p512, (1993).

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 1 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


ABS Resins; Molded, Extruded	Medium impact	5—20
	High impact	5—50
	Very high impact	20—50
	Low temperature impact	30—200
	Heat resistant	20
Acrylics; Cast, Molded, Extruded	Cast Resin Sheets, Rods:
	General purpose, type I	2—7
	General purpose, type II	2—7
	Moldings:
	Grades 5, 6, 8	3—5
	High impact grade	>25
	Chlorinated Polymers
	Chlorinated polyether	130

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 2 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


Polycarbonates	Polycarbonate	110
	Polycarbonate (40% glass ﬁber reinforced)	0—5
Fluorocarbons; Molded,Extruded	Polytriﬂuoro chloroethylene (PTFCE)	125—175
	Polytetraﬂuoroethylene (PTFE)	250—350
	Ceramic reinforced (PTFE)	10—200
	Fluorinated ethylene propylene(FEP)	250—330
	Polyvinylidene— ﬂuoride (PVDF)	200—300
Epoxies; Cast, Molded, Reinforced	Standard epoxies (diglycidyl ethers of bisphenol A)
	Cast rigid	4.4
	Cast ﬂexible	1.5-60

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 3 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


Epoxies—Molded, Extruded	High performance resins (cycloaliphatic diepoxides)
	Cast, rigid	2—5
	Epoxy novolacs
	Glass cloth laminate	2.2—4.8
Melamines; Molded	Cellulose electrical	0.6
Nylons; Molded, Extruded	Type 6
	General purpose	30—100
	Glass ﬁber (30%) reinforced	2.2—3.6
	Cast	20
	Flexible copolymers	200—320
	Type 8	400
	Type 11	100—120
	Type 12	120—350

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 4 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


	6/6 Nylon
	General purpose molding	15—300
	Glass ﬁber reinforced	1.8—2.2
	Glass ﬁber Molybdenum disulﬁde ﬁlled	3
	General purpose extrusion	90—240
Nylons; Molded, Extruded (Con’t)	6/10 Nylon
	General purpose	85—220
	Glass ﬁber (30%) reinforced	1.9
Phenolics; Molded	Type and ﬁller
	General: woodﬂour and ﬂock	0.4—0.8
	High shock: chopped fabric or cord	0.37—0.57
	Very high shock: glass ﬁber	0.2
	Rubber phenolic—woodﬂour or ﬂock	0.75—2.25
ABS–Polycarbonate Alloy	ABS–Polycarbonate Alloy	110

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 5 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


PVC–Acrylic Alloy	PVC–acrylic sheet	>100
	PVC–acrylic injection molded	150
Polymides	Unreinforced	<1
	Unreinforced 2nd value	1.2
	Glass reinforced	<1
Polyacetals	Homopolymer:
	Standard	25
	20% glass reinforced	7
	22% TFE reinforced	12
	Copolymer:
	Standard	60—75
	25% glass reinforced	3
	High ﬂow	40

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 6 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


Polyester; Thermoplastic	Injection Moldings:
	General purpose grade	300
	Glass reinforced grades	1—5
	Glass reinforced self extinguishing	5
	General purpose grade	250
	Glass reinforced grade	<5
	Asbestos—ﬁlled grade	<5
Polyesters: Thermosets	Cast polyyester
	Rigid	1.7—2.6
	Flexible	25—300
Reinforced polyester moldings	High strength (glass ﬁbers)	0.3—0.5
Phenylene Oxides	SE—100	50
	SE—1	60
	Glass ﬁber reinforced	4—6

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 7 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


Phenylene oxides (Noryl)	Standard	50—100
Polyarylsulfone	Polyarylsulfone	15—40
Polypropylene	General purpose	100—600
	High impact	30—>200
Polypropylene (Con’t)	Asbestos ﬁlled	3—20
	Glass reinforced	2—4
	Flame retardant	3—15
Polyphenylene sulﬁde	Standard	3
	40% glass reinforced	3—9
Polyethylenes; Molded, Extruded	Type I—lower density (0.910—0.925)	(ASTM D412)
	Melt index 0.3—3.6	500—725
	Melt index 6—26	125—675
	Melt index 200	80—100

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 8 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


	Type II—medium density (0.926—0.940)
	Melt index 20	200
	Melt index l.0—1.9	200—425
Polyethylenes; Molded, Extruded (Con’t)	Type III—higher density (0.941—0.965)
	Melt index 0.2—0.9	700—1,000
	Melt Melt index 0.l—12.0	50—l,000
	Melt index 1.5—15	100—700
	High molecular weight	400
Oleﬁn Copolymers; Molded	EEA (ethylene ethyl acrylate)	650
	EVA (ethylene vinyl acetate)	650
	Ethylene butene	20
	Ionomer	450
	Polyallomer	300—400

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 9 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


Polystyrenes; Molded	General purpose	1.0—2.3
	Medium impact	3.0—40
	Glass ﬁber -30% reinforced	1.1
	Styrene acrylonitrile (SAN)	0.5—4.5
	Glass ﬁber (30%) reinforced SAN	1.4—1.6
Polyvinyl Chloride And Copolymers; Molded,	Nonrigid—general	200—450
Extruded	Nonrigid—general	200—450
Extruded
	Nonrigid—electrical	220—360
	Rigid—normal impact	1—10
	Vinylidene chloride	15—30

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 269. TOTAL ELONGATION OF POLYMERS

(SHEET 10 OF 10)

		Elongation (in 2 in.), (ASTM
		D638)
Class	Polymer	(%)


Silicones; Molded, Laminated		(ASTM D651)
	Fibrous (glass) reinforced silicones	<3
	Granular (silica) reinforced silicones	<3
Ureas; Molded	Alpha—cellulose ﬁlled (ASTM Type l)	1

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 270. ELONGATION AT YIELD FOR POLYMERS

(SHEET 1 OF 3)

		Elongation at Yield, (ASTM D638)
Class	Polymer	(%)


Chlorinated polyether	Chlorinated polyether	15
Polycarbonates	Polycarbonate	5
Nylons; Molded, Extruded	Type 6
	Cast	5
	Type 12	5.8
	6/6 Nylon:
	General purpose molding	5—25
	General purpose extrusion	5—30
	6/10 Nylon:
	General purpose	5—30

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 270. ELONGATION AT YIELD FOR POLYMERS

(SHEET 2 OF 3)

		Elongation at Yield, (ASTM D638)
Class	Polymer	(%)


Polyacetals	Homopolymer:
	Standard	12
	Copolymer:
	Standard	12
	25% glass reinforced	3
	High ﬂow	12
Phenylene oxides (Noryl)	Standard	5.6
	Glass ﬁber reinforced	1.6—2
Polyarylsulfone	Polyarylsulfone	6.5—13
Polypropylene:	General purpose	9—15
	High impact	7—13
	Asbestos ﬁlled	5
Polyphenylene sulﬁde:	Standard	1.6
	40% glass reinforced	1.25

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 270. ELONGATION AT YIELD FOR POLYMERS

(SHEET 3 OF 3)

		Elongation at Yield, (ASTM D638)
Class	Polymer	(%)


Polystyrenes; Molded	General purpose	1.0—2.3
	Medium impact	1.2—3.0
	High impact	1.5—2.0
	Glass ﬁber -30% reinforced	1.1
	Glass ﬁber (30%) reinforced SAN	1.4—1.6

Source: data compiled by J.S. Park from Charles T. Lynch, CRC Handbook of Materials Science, Vol. 3, CRC Press, Boca Raton, Florida, 1975 and

Engineered Materials Handbook, Vol.2, Engineering Plastics, ASM International, Metals Park, Ohio, 1988.

Table 271. ULTIMATE TENSILE ELONGATION OF

FIBERGLASS REINFORCED PLASTICS

		Glass	Ultimate
		fiber content	tensile elongation
Class	Material	(wt%)	(%)


Glass ﬁber reinforced	Sheet molding compound (SMC)	15 to 30	0.3 to 1.5
thermosets	Sheet molding compound (SMC)	15 to 30	0.3 to 1.5
thermosets
	Bulk molding compound(BMC)	15 to 35	0.3 to 5
	Preform/mat(compression molded)	25 to 50	1 to 2
	Cold press molding–polyester	20 to 30	1 to 2
	Spray–up–polyester	30 to 50	1.0 to 1.2
	Filament wound–epoxy	30 to 80	1.6 to 2.8
	Rod stock–polyester	40 to 80	1.6 to 2.5
	Molding compound–phenolic	5 to 25	0.25 to 0.6
Glass–ﬁber–reinforced	Acetal	20 to 40	2
thermoplastics	Acetal	20 to 40	2
thermoplastics
	Nylon	6 to 60	2 to 10
	Polycarbonate	20 to 40	2
	Polyethylene	10 to 40	1.5 to 3.5
	Polypropylene	20 to 40	1 to 3
	Polystyrene	20 to 35	1.0 to 1.4
	Polysulfone	20 to 40	2 to 3
	ABS(acrylonitrile butadiene styrene)	20 to 40	3 to 3.4
	PVC (polyvinyl chloride)	15 to 35	2 to 4
	Polyphenylene oxide(modiﬁed)	20 to 40	1.7 to 5
	SAN (styrene acrylonitrile)	20 to 40	1.1 to 1.6
	Thermoplastic polyester	20 to 35	1 to 5

To convert (ksi) to (Mpa), multiply by 6.89

Data from ASM Engineering Materials Reference Book, Second Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p106, (1994).

Table 272. TOTAL STRAIN OF

SILICON CARBIDE SCS–2–AL

Fiber orientation	No. of plies	Total Strain


0°	6, 8, 12	0.89
90°	6, 12,40	0.08
[0°/90°/0°/90°]s	8	0.90
[02 °99°20°]s	8	0.92
[902/90°/90°]s	8	1.01
± 45°	8, 12, 40	10.6
[0°±45°/0°]s+2s	8, 16	0.86
[0°±45°/90°]s	8	1.0

Data from ASM Engineering Materials Reference Book, Second Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p149,(1994).

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