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    1. Распределение циркуляции по размаху плоского крыла.

Применяем следующие обозначения:

L– размах крыла;

Lц– размах центроплана;

 – сужение крыла;

– относительная координатаz.

Таблица 4.6. Распределение циркуляции при Lц/L=0.5.

0.0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1.0

1.2

1.172

1.172

1.170

1.159

1.137

1.094

1.029

0.946

0.941

0.693

0.0

1.4

1.179

1.179

1.177

1.166

1.142

1.097

1.029

0.941

0.832

0.676

0.0

1.6

1.186

1.186

1.184

1.173

1.147

1.100

1.029

0.936

0.823

0.659

0.0

1.8

1.193

1.193

1.191

1.180

1.152

1.103

1.029

0.931

0.814

0.642

0.0

2.0

1.200

1.200

1.196

1.186

1.158

1.107

1.029

0.927

0.804

0.634

0.0

2.2

1.207

1.207

1.205

1.192

1.164

1.111

1.029

0.923

0.794

0.626

0.0

2.4

1.214

1.214

1.211

1.199

1.169

1.114

1.028

0.922

0.784

0.608

0.0

2.6

1.220

1.220

1.218

1.205

1.174

1.117

1.028

0.913

0.775

0.596

0.0

2.8

1.227

1.227

1.224

1.211

1.180

1.120

1.028

0.908

0.765

0.583

0.0

3.0

1.233

1.233

1.231

1.218

1.185

1.124

1.028

0.904

0.755

0.571

0.0

3.2

1.237

1.237

1.235

1.222

1.188

1.126

1.028

0.901

0.749

0.563

0.0

3.4

1.242

1.242

1.239

1.225

1.191

1.127

1.028

0.899

0.743

0.555

0.0

3.6

1.256

1.256

1.243

1.229

1.194

1.128

1.028

0.896

0.738

0.547

0.0

3.8

1.250

1.250

1.247

1.232

1.197

1.130

1.028

0.893

0.732

0.538

0.0

4.0

1.254

1.254

1.251

1.236

1.200

1.132

1.028

0.891

0.726

0.530

0.0

4.2

1.257

1.257

1.253

1.238

1.202

1.133

1.028

0.890

0.723

0.525

0.0

4.4

1.259

1.259

1.255

1.241

1.204

1.135

1.029

0.888

0.719

0.520

0.0

4.6

1.262

1.262

1.257

1.243

1.206

1.136

1.029

0.887

0.716

0.515

0.0

4.8

1.265

1.265

1.259

1.145

1.208

1.137

1.029

0.885

0.713

0.510

0.0

5.0

1.267

1.267

1.262

1.248

1.210

1.139

1.029

0.884

0.709

0.505

0.0

Таблица 4.7. Распределение циркуляции при Lц/L=0.25.

0.0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1.0

1.2

1.209

1.208

1.191

1.174

1.124

1.073

1.028

0.923

0.839

0.688

0.0

1.4

1.222

1.220

1.202

1.178

1.130

10.72

1.019

0.916

0.826

0.675

0.0

1.6

1.235

1.231

1.213

1.182

1.136

10.74

1.010

0.909

0.813

0.622

0.0

1.8

1.248

1.242

1.224

1.191

1.141

1.075

1.001

0.902

0.800

0.649

0.0

2.0

1.260

1.254

1.234

1.199

1.146

1.076

0.991

0.895

0.787

0.635

0.0

2.2

1.272

1.266

1.144

1.207

1.151

1.077

0.987

0.888

0.774

0.621

0.0

2.4

1.284

1.277

1.255

1.215

1.156

1.078

0.984

0.882

0.762

0.607

0.0

2.6

1.297

1.289

1.265

1.224

1.161

1.079

0.980

0.875

0.749

0.594

0.0

2.8

1.309

1.300

1.276

1.232

1.166

1.080

0.977

0.867

0.737

0.580

0.0

3.0

1.321

1.312

1.286

1.240

1.171

1.081

0.973

0.862

0.724

0.566

0.0

3.2

1.328

1.319

1.292

1.245

1.174

1.082

0.971

0.855

0.717

0.558

0.0

3.4

1.335

1.325

1.195

1.149

1.177

1.083

0.969

0.849

0.710

0.549

0.0

3.6

1.341

1.332

1.303

1.254

1.180

1.093

0.967

0.842

0.702

0.541

0.0

3.8

1.348

1.338

1.309

1.258

1.183

1.084

0.965

0.836

0.695

0.532

0.0

4.0

1.355

1.345

1.315

1.263

1.186

1.085

0.963

0.829

0.688

0.524

0.0

4.2

1.360

1.349

1.320

1.266

1.188

1.085

0.962

0.826

0.683

0.513

0.0

4.4

1.365

1.354

1.325

1.269

1.191

1.085

0.961

0.823

0.678

0.501

0.0

4.6

1.369

1.358

1.331

1.273

1.193

1.085

0.960

0.82

0.672

0.490

0.0

4.8

1.374

1.363

1.336

1.276

1.196

1.085

0.959

0.817

0.667

0.478

0.0

5.0

1.379

1.367

1.341

1.278

1.198

1.085

0.958

0.814

0.66

0.467

0.0

Таблица 4.8. Распределение циркуляции при Lц/L=0.0.

0.0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1.0

1.0

1.129

1.126

1.120

1.110

1.096

1.077

1.046

0.995

0.914

0.760

0.0

1.2

1.158

1.153

1.143

1.126

1.103

1.073

1.033

0.976

0.892

0.738

0.0

1.4

1.186

1.180

1.166

1.142

1.110

1.070

1.020

0.957

0.870

0.716

0.0

1.6

1.215

1.208

1.190

1.157

1.116

1.066

1.007

0.937

0.847

0.695

0.0

1.8

1.243

1.235

1.213

1.173

1.123

1.063

0.994

0.918

0.825

0.673

0.0

2.0

1.272

1.262

1.236

1.189

1.130

1.059

0.981

0.899

0.803

0.651

0.0

2.2

1.286

1.276

1.247

1.196

1.134

1.059

0.976

0.390

0.791

0.643

0.0

2.4

1.301

1.289

1.258

1.203

1.137

1.058

0.971

0.881

0.779

0.634

0.0

2.6

1.315

1.303

1.269

1.109

1.141

1.058

0.967

0.872

0.767

0.626

0.0

2.8

1.330

1.316

1.280

1.216

1.144

1.057

0.962

0.863

0.755

0.617

0.0

3.0

1.344

1.330

1.291

1.113

1.148

1.057

0.957

0.854

0.743

0.609

0.0

3.2

1.352

1.338

1.298

1.229

1.150

1.056

0.954

0.849

0.735

0.596

0.0

3.4

1.361

1.346

1.305

1.235

1.153

1.056

0.951

0.843

0.728

0.583

0.0

3.6

1.369

1.354

1.311

1.240

1.155

1.055

0.948

0.838

0.720

0.560

0.0

3.8

1.378

1.362

1.318

1.246

1.158

1.055

0.945

0.832

0.713

0.556

0.0

4.0

1.386

1.30

1.325

1.252

1.160

1.054

0.942

0.827

0.705

0.543

0.0

4.2

1.92

1.376

1.330

1.256

1.162

1.054

0.940

0.824

0.700

0.539

0.0

4.4

1.398

1.382

1.335

1.260

1.164

1.055

0.939

0.820

0.694

0.531

0.0

4.6

1.404

1.387

1.339

1.263

1.167

1.055

0.937

0.817

0.689

0.524

0.0

4.8

1.410

1.393

1.334

1.267

1.169

1.056

0.936

0.813

0.683

0.518

0.0

5.0

1.416

1.399

1.349

1.271

1.171

1.056

0.934

0.810

0.678

0.512

0.0