NACA 4412 Coordinates

Name = naca-4412 Mach = 0; Re = 25000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition und effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. C.P. [?] [-] [-] [-] [-] [-] [-] -15.0 15.0 -0.52 0.520 0 0.202 .2027 72 -0.0 -0.027 27 0.92 0.922 2 0.00 0.005 5 0.198 -14.5 14.5 -0.50 0.500 0 0.187 .1875 50 -0.0 -0.030 30 0.91 0.915 5 0.00 0.005 5 0.191 -14.0 14.0 -0.47 0.478 8 0.162 .1627 79 -0.0 -0.032 32 0.91 0.910 0 0.00 0.006 6 0.182 -13.5 13.5 -0.45 0.454 4 0.157 .1570 04 -0.0 -0.035 35 0.90 0.904 4 0.00 0.006 6 0.173 -13.0 13.0 -0.42 0.428 8 0.142 .1424 46 -0.0 -0.038 38 0.89 0.899 9 0.00 0.006 6 0.161 -12.5 12.5 -0.40 0.400 0 0.140 .1404 49 -0.0 -0.041 41 0.89 0.893 3 0.00 0.006 6 0.148 -12.0 12.0 -0.37 0.371 1 0.124 .1243 30 -0.0 -0.044 44 0.88 0.889 9 0.00 0.007 7 0.133 -11.5 11.5 -0.33 0.339 9 0.114 .1140 08 -0.0 -0.046 46 0.88 0.880 0 0.00 0.007 7 0.114 -11.0 11.0 -0.30 0.306 6 0.108 .1084 44 -0.0 -0.049 49 0.87 0.871 1 0.00 0.008 8 0.089 -10.5 10.5 -0.27 0.271 1 0.106 .1065 56 -0.0 -0.052 52 0.86 0.862 2 0.00 0.008 8 0.058 -10.0 10.0 -0.23 0.236 6 0.093 .0936 61 -0.0 -0.055 55 0.85 0.854 4 0.00 0.008 8 0.018 -9.5 9.5 -0.19 0.199 9 0.08 0.0873 737 7 -0.0 -0.058 58 0. 0.846 846 0.00 0.009 9 -0.040 -9.0 9.0 -0.16 0.162 2 0.08 0.0803 033 3 -0.0 -0.061 61 0. 0.833 833 0.00 0.009 9 -0.126 -8.5 8.5 -0.12 0.123 3 0.07 0.0779 791 1 -0.0 -0.064 64 0. 0.823 823 0.01 0.010 0 -0.269 -8.0 8.0 -0.08 0.083 3 0.06 0.0696 965 5 -0.0 -0.066 66 0. 0.814 814 0.01 0.011 1 -0.548 -7.5 7.5 -0.04 0.043 3 0.06 0.0659 596 6 -0.0 -0.069 69 0. 0.801 801 0.01 0.012 2 -1.355 -7.0 7.0 -0.00 0.003 3 0.05 0.0599 993 3 -0.0 -0.072 72 0. 0.788 788 0.01 0.013 3 -27.183 -6.5 6.5 -0.29 0.293 3 0.05 0.0550 500 0 -0.0 -0.075 75 0. 0.777 777 0.01 0.014 4 -0.007 -6.0 6.0 -0.22 0.225 5 0.05 0.0518 186 6 -0.0 -0.078 78 0. 0.761 761 0.01 0.015 5 -0.098 -5.5 5.5 -0.15 0.158 8 0.05 0.0504 043 3 -0.0 -0.081 81 0. 0.746 746 0.01 0.017 7 -0.265 -5.0 5.0 -0.09 0.091 1 0.04 0.0469 697 7 -0.0 -0.084 84 0. 0.730 730 0.01 0.019 9 -0.673 -4.5 4.5 -0.02 0.025 5 0.04 0.0450 509 9 -0.0 -0.087 87 0. 0.713 713 0.02 0.023 3 -3.194 -4.0 0.040 0.04165 -0.090 0. 0.693 0.028 2.519 -3.5 0.104 0.04005 -0.093 0. 0.674 0.034 1.147 -3.0 0.167 0.03810 -0.096 0. 0.652 0.043 0.825 -2.5 0.227 0.03258 -0.099 0. 0.629 0.058 0.685

model = 1; Aspect Ratio = 0; gro S.U.

S.L.

L/D

A.C.

[-]

[-]

[-]

[-]

1.00 1.000 0

0.00 0.008 8

-2.5 -2.563 63

0.3 0.388

1.00 1.000 0

0.00 0.008 8

-2.6 -2.666 66

0.3 0.379

1.00 1.000 0

0.00 0.008 8

-2.9 -2.933 33

0.3 0.370

1.00 1.000 0

0.00 0.008 8

-2.8 -2.892 92

0.3 0.363

1.00 1.000 0

0.00 0.008 8

-3.0 -3.006 06

0.3 0.353

1.00 1.000 0

0.00 0.009 9

-2.8 -2.850 50

0.3 0.348

1.00 1.000 0

0.00 0.009 9

-2.9 -2.983 83

0.3 0.342

1.00 1.000 0

0.00 0.009 9

-2.9 -2.974 74

0.3 0.337

1.00 1.000 0

0.01 0.010 0

-2.8 -2.821 21

0.3 0.334

1.00 1.000 0

0.01 0.011 1

-2.5 -2.547 47

0.3 0.332

1.00 1.000 0

0.01 0.011 1

-2.5 -2.524 24

0.3 0.330

1.00 1.000 0

0.01 0.012 2

-2.2 -2.279 79

0.3 0.327 27

1.00 1.000 0

0.01 0.013 3

-2.0 -2.011 11

0.3 0.326 26

1.00 1.000 0

0.01 0.014 4

-1.5 -1.572 72

0.3 0.325 25

1.00 1.000 0

0.01 0.014 4

-1.1 -1.196 96

0.3 0.324 24

1.00 1.000 0

0.01 0.016 6

-0.6 -0.656 56

0.3 0.323 23

1.00 1.000 0

0.01 0.017 7

-0.0 -0.044 44

0.2 0.226 26

1.00 1.000 0

0.01 0.019 9

-5.3 -5.328 28

0.2 0.223 23

1.00 1.000 0

0.02 0.021 1

-4.3 -4.344 44

0.2 0.294 94

1.00 1.000 0

0.02 0.024 4

-3.1 -3.132 32

0.2 0.295 95

1.00 1.000 0

0.02 0.028 8

-1.9 -1.944 44

0.2 0.295 95

1.00 1.000 0

0.03 0.034 4

-0.5 -0.562 62

0.2 0.295 95

1.000

0.043

0.955

0.296

0.921

0.058

2.594

0.296

0.919

0.090

4.380

0.296

0.917

0.304

6.973

0.380

-2.0 0.644 -1.5 0.577 -1.0 0.530 -0.5 0.496 0.0 0.470 0.5 0.468 1.0 0.452 1.5 0.439 2.0 0.430 2.5 0.423 3.0 0.418 3.5 0.415 4.0 0.412 4.5 0.410 5.0 0.407 5.5 0.405 6.0 0.403 6.5 0.401 7.0 0.398 7.5 0.395 8.0 0.368 8.5 0.369 9.0 0.403 9.5 0.399 10.0 0.397 10.5 0.395 11.0 0.394 11.5 0.393 12.0 0.393 12.5 0.393

0.282

0.02768 -0.111

0.603

0.084

0.917

0.966

10.185

0.365

0.343

0.02693 -0.112

0.574

0.120

0.916

0.967

12.736

0.269

0.404

0.02730 -0.113

0.541

0.170

0.918

0.968

14.800

0.268

0.465

0.02783 -0.114

0.502

0.249

0.921

0.967

16.702

0.269

0.526

0.02902 -0.116

0.459

0.881

1.000

0.962

18.114

0.286

0.536

0.02923 -0.117

0.431

0.912

0.919

0.962

18.341

0.299

0.587

0.02947 -0.119

0.417

0.940

0.905

0.962

19.927

0.284

0.636

0.03027 -0.120

0.407

0.961

0.890

0.961

21.021

0.291

0.682

0.03090 -0.122

0.401

0.961

0.868

0.962

22.054

0.302

0.723

0.03205 -0.125

0.395

0.961

0.842

0.962

22.562

0.317

0.760

0.03350 -0.128

0.389

0.961

0.809

0.963

22.695

0.335

0.795

0.03515 -0.131

0.382

0.962

0.773

0.963

22.616

0.344

0.831

0.03713 -0.134

0.372

0.962

0.740

0.963

22.372

0.352

0.864

0.03969 -0.138

0.361

0.961

0.705

0.962

21.776

0.354

0.901

0.04154 -0.142

0.348

0.961

0.677

0.962

21.700

0.352

0.937

0.04367 -0.146

0.334

0.962

0.648

0.963

21.456

0.353

0.974

0.04621 -0.149

0.318

0.962

0.623

0.963

21.083

0.343

1.015

0.04881 -0.153

0.299

0.961

0.606

0.962

20.796

0.334

1.057

0.05137 -0.156

0.277

0.961

0.593

0.963

20.571

0.326

1.102

0.05331 -0.159

0.250

0.963

0.589

0.964

20.677

0.226

1.282

0.04884 -0.151

0.040

0.961

0.779

0.963

26.240

0.231

1.306

0.05134 -0.156

0.020

0.962

0.746

0.962

25.437

0.093

1.135

0.07101 -0.174

0.015

0.962

0.043

0.962

15.977

0.078

1.184

0.07279 -0.176

0.012

0.963

0.026

0.964

16.268

0.313

1.223

0.07741 -0.179

0.010

0.962

0.019

0.963

15.805

0.332

1.258

0.08370 -0.182

0.009

0.962

0.016

0.963

15.028

0.345

1.288

0.08806 -0.186

0.008

0.962

0.014

0.963

14.630

0.353

1.318

0.09504 -0.189

0.006

0.963

0.012

0.964

13.868

0.360

1.345

0.09923 -0.192

0.006

0.963

0.010

0.964

13.550

0.376

1.368

0.10703 -0.195

0.005

0.963

0.009

0.965

12.777

0.398

13.0 0.393 13.5 0.393 14.0 0.394 14.5 0.395 15.0 0.396

1.387

0.11790 -0.198

0.005

0.964

0.008

0.965

11.764

0.417

1.405

0.12181 -0.201

0.005

0.964

0.007

0.965

11.533

0.443

1.419

0.13665 -0.204

0.004

0.964

0.007

0.965

10.386

0.501

1.430

0.15064 -0.207

0.004

0.964

0.007

0.965

9.492

0.551

1.440

0.15874 -0.211

0.004

0.964

0.006

0.965

9.071

0.557

Name = naca-4412 Mach = 0; Re = 50000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition und effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. C.P. [?] [-] [-] [-] [-] [-] [-] -15.0 -0.519 0.15952 -0.027 0.922 0.005 0.198 -14.5 -0.499 0.14658 -0.030 0.915 0.005 0.191 -14.0 -0.477 0.13387 -0.032 0.910 0.006 0.182 -13.5 -0.453 0.13539 -0.035 0.904 0.006 0.173 -13.0 -0.428 0.12118 -0.038 0.899 0.006 0.161 -12.5 -0.400 0.10777 -0.041 0.893 0.006 0.148 -12.0 -0.370 0.10566 -0.043 0.889 0.007 0.133 -11.5 -0.339 0.09463 -0.046 0.880 0.007 0.113 -11.0 -0.305 0.09058 -0.049 0.871 0.008 0.089 -10.5 -0.271 0.08195 -0.052 0.862 0.008 0.058 -10.0 -0.236 0.07807 -0.055 0.854 0.008 0.017 -9.5 -0.199 0.07190 -0.058 0.846 0.009 -0.041 -9.0 -0.161 0.06668 -0.061 0.833 0.009 -0.127 -8.5 -0.122 0.06371 -0.064 0.823 0.010 -0.271 -8.0 -0.083 0.05850 -0.066 0.814 0.011 -0.555 -7.5 -0.042 0.05544 -0.069 0.801 0.012 -1.386 -7.0 -0.001 0.05215 -0.072 0.788 0.013 -53.649 -6.5 -0.293 0.04773 -0.075 0.777 0.014 -0.007 -6.0 -0.225 0.04450 -0.078 0.761 0.015 -0.097 -5.5 -0.158 0.04222 -0.081 0.746 0.017 -0.264 -5.0 -0.091 0.03962 -0.084 0.730 0.019

model = 1; Aspect Ratio = 0; gro S.U.

S.L.

L/D

A.C.

[-]

[-]

[-]

[-]

1.000

0.008

-3.254

0.388

1.000

0.008

-3.406

0.379

1.000

0.009

-3.563

0.369

1.000

0.009

-3.348

0.362

1.000

0.009

-3.528

0.355

1.000

0.009

-3.712

0.348

1.000

0.009

-3.504

0.341

1.000

0.010

-3.578

0.337

1.000

0.011

-3.372

0.335

1.000

0.011

-3.312

0.332

1.000

0.011

-3.020

0.329

1.000

0.013

-2.762

0.327

1.000

0.013

-2.414

0.326

1.000

0.014

-1.914

0.324

1.000

0.016

-1.410

0.324

1.000

0.017

-0.765

0.322

1.000

0.019

-0.026

0.226

1.000

0.021

-6.138

0.224

1.000

0.024

-5.061

0.294

1.000

0.028

-3.740

0.294

1.000

0.032

-2.303

0.295

-0.673 -4.5 -3.190 -4.0 2.515 -3.5 1.144 -3.0 0.932 -2.5 0.748 -2.0 0.644 -1.5 0.577 -1.0 0.530 -0.5 0.496 0.0 0.470 0.5 0.449 1.0 0.431 1.5 0.417 2.0 0.405 2.5 0.395 3.0 0.395 3.5 0.393 4.0 0.388 4.5 0.384 5.0 0.380 5.5 0.377 6.0 0.375 6.5 0.373 7.0 0.371 7.5 0.369 8.0 0.360 8.5 0.360 9.0 0.361 9.5 0.363 10.0

-0.025

0.03746 -0.087

0.713

0.023

1.000

0.042

-0.676

0.294

0.040

0.03460 -0.090

0.693

0.028

1.000

0.063

1.148

0.289

0.103

0.03028 -0.092

0.674

0.034

1.000

0.191

3.404

0.407

0.160

0.02127 -0.109

0.652

0.043

1.000

0.966

7.503

0.401

0.221

0.02101 -0.110

0.629

0.058

1.000

0.967

10.508

0.268

0.282

0.02083 -0.111

0.603

0.084

1.000

0.967

13.534

0.268

0.343

0.01957 -0.112

0.574

0.120

1.000

0.968

17.525

0.268

0.404

0.01991 -0.113

0.541

0.170

1.000

0.968

20.289

0.268

0.465

0.02150 -0.114

0.502

0.249

1.000

0.968

21.621

0.269

0.526

0.02060 -0.116

0.459

0.881

1.000

0.962

25.508

0.267

0.586

0.02041 -0.116

0.431

0.912

1.000

0.962

28.735

0.265

0.647

0.02200 -0.117

0.417

0.940

1.000

0.962

29.413

0.266

0.708

0.02142 -0.118

0.407

0.961

1.000

0.961

33.048

0.266

0.769

0.02139 -0.119

0.401

0.961

1.000

0.962

35.921

0.266

0.829

0.02147 -0.120

0.395

0.961

1.000

0.962

38.622

0.300

0.849

0.02368 -0.123

0.389

0.961

0.944

0.963

35.851

0.360

0.882

0.02466 -0.126

0.382

0.962

0.909

0.963

35.793

0.311

0.931

0.02551 -0.128

0.372

0.962

0.894

0.963

36.484

0.298

0.977

0.02702 -0.131

0.361

0.961

0.880

0.962

36.170

0.303

1.023

0.02793 -0.133

0.348

0.961

0.864

0.962

36.631

0.309

1.067

0.02899 -0.136

0.334

0.962

0.848

0.963

36.811

0.315

1.110

0.03039 -0.139

0.318

0.962

0.831

0.963

36.515

0.316

1.154

0.03211 -0.142

0.299

0.961

0.818

0.962

35.948

0.315

1.198

0.03392 -0.145

0.277

0.961

0.805

0.963

35.327

0.314

1.243

0.03540 -0.147

0.250

0.963

0.796

0.964

35.121

0.260

1.331

0.03883 -0.146

0.040

0.961

0.842

0.963

34.281

0.269

1.364

0.04126 -0.150

0.020

0.962

0.820

0.962

33.073

0.385

1.391

0.04358 -0.154

0.015

0.962

0.794

0.962

31.918

0.463

1.409

0.04611 -0.159

0.012

0.963

0.759

0.964

30.567

0.112

1.202

0.06951 -0.180

0.010

0.962

0.039

0.963

17.297

0.103

0.400 10.5 0.396 11.0 0.395 11.5 0.394 12.0 0.393 12.5 0.393 13.0 0.393 13.5 0.393 14.0 0.394 14.5 0.395 15.0 0.396

1.250

0.07224 -0.183

0.009

0.962

0.021

0.963

17.304

0.320

1.282

0.07642 -0.186

0.008

0.962

0.018

0.963

16.773

0.346

1.314

0.08002 -0.189

0.006

0.963

0.014

0.964

16.417

0.353

1.341

0.08443 -0.192

0.006

0.963

0.012

0.964

15.884

0.371

1.365

0.09102 -0.195

0.005

0.963

0.011

0.965

14.993

0.391

1.385

0.09723 -0.198

0.005

0.964

0.009

0.965

14.245

0.412

1.403

0.10152 -0.201

0.005

0.964

0.008

0.965

13.820

0.443

1.417

0.11201 -0.204

0.004

0.964

0.008

0.965

12.654

0.490

1.429

0.11561 -0.207

0.004

0.964

0.007

0.965

12.360

0.539

1.439

0.12519 -0.211

0.004

0.964

0.006

0.965

11.493

0.563

Name = naca-4412 Mach = 0; Re = 75000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition und effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. C.P. [?] [-] [-] [-] [-] [-] [-] -15.0 -0.519 0.14735 -0.027 0.922 0.005 0.198 -14.5 -0.499 0.13383 -0.030 0.915 0.005 0.191 -14.0 -0.476 0.12187 -0.032 0.910 0.006 0.182 -13.5 -0.453 0.11003 -0.035 0.904 0.006 0.173 -13.0 -0.428 0.10182 -0.038 0.899 0.006 0.161 -12.5 -0.399 0.09963 -0.041 0.893 0.006 0.148 -12.0 -0.370 0.09010 -0.043 0.889 0.007 0.133 -11.5 -0.338 0.08649 -0.046 0.880 0.007 0.113 -11.0 -0.305 0.08264 -0.049 0.871 0.008 0.089 -10.5 -0.271 0.07546 -0.052 0.862 0.008 0.058 -10.0 -0.235 0.07100 -0.055 0.854 0.008 0.017 -9.5 -0.198 0.06506 -0.058 0.846 0.009 -0.041 -9.0 -0.160 0.06062 -0.061 0.833 0.009 -0.128 -8.5 -0.122 0.05721 -0.064 0.823 0.010 -0.272 -8.0 -0.082 0.05360 -0.066 0.814 0.011 -0.563

model = 1; Aspect Ratio = 0; gro S.U.

S.L.

L/D

A.C.

[-]

[-]

[-]

[-]

1.000

0.009

-3.519

0.388

1.000

0.009

-3.727

0.379

1.000

0.009

-3.910

0.371

1.000

0.009

-4.119

0.364

1.000

0.009

-4.199

0.353

1.000

0.009

-4.009

0.348

1.000

0.009

-4.109

0.341

1.000

0.011

-3.910

0.336

1.000

0.011

-3.690

0.335

1.000

0.011

-3.591

0.332

1.000

0.012

-3.314

0.329

1.000

0.013

-3.045

0.327

1.000

0.014

-2.647

0.326

1.000

0.015

-2.125

0.324

1.000

0.017

-1.524

0.323

-7.5 -1.418 -7.0 0.250 -6.5 -0.007 -6.0 -0.097 -5.5 -0.264 -5.0 -0.671 -4.5 -3.182 -4.0 3.103 -3.5 1.345 -3.0 0.932 -2.5 0.748 -2.0 0.644 -1.5 0.577 -1.0 0.530 -0.5 0.496 0.0 0.470 0.5 0.449 1.0 0.431 1.5 0.417 2.0 0.405 2.5 0.395 3.0 0.386 3.5 0.379 4.0 0.372 4.5 0.366 5.0 0.372 5.5 0.369 6.0 0.366 6.5 0.363 7.0 0.361

-0.042

0.05063 -0.069

0.801

0.012

1.000

0.018

-0.821

0.323

-0.001

0.04741 -0.072

0.788

0.013

1.000

0.020

-0.013

0.227

-0.293

0.04412 -0.075

0.777

0.014

1.000

0.024

-6.639

0.224

-0.225

0.04125 -0.078

0.761

0.015

1.000

0.027

-5.458

0.294

-0.158

0.03896 -0.081

0.746

0.017

1.000

0.032

-4.051

0.293

-0.091

0.03673 -0.084

0.730

0.019

1.000

0.043

-2.482

0.293

-0.025

0.03496 -0.087

0.713

0.023

1.000

0.065

-0.723

0.426

0.037

0.01707 -0.107

0.693

0.028

1.000

0.966

2.189

0.420

0.098

0.01712 -0.108

0.674

0.034

1.000

0.967

5.750

0.268

0.160

0.01878 -0.109

0.652

0.043

1.000

0.967

8.499

0.268

0.221

0.01847 -0.110

0.629

0.058

1.000

0.968

11.955

0.268

0.282

0.01805 -0.111

0.603

0.084

1.000

0.968

15.621

0.268

0.343

0.01712 -0.112

0.574

0.120

1.000

0.969

20.030

0.268

0.404

0.01749 -0.113

0.541

0.170

1.000

0.969

23.100

0.268

0.465

0.01823 -0.114

0.502

0.249

1.000

0.969

25.502

0.268

0.526

0.01758 -0.116

0.459

0.881

1.000

0.963

29.899

0.267

0.586

0.01796 -0.116

0.431

0.912

1.000

0.962

32.657

0.265

0.647

0.01802 -0.117

0.417

0.940

1.000

0.962

35.925

0.266

0.708

0.01818 -0.118

0.407

0.961

1.000

0.961

38.935

0.266

0.769

0.01763 -0.119

0.401

0.961

1.000

0.962

43.588

0.266

0.829

0.01849 -0.120

0.395

0.961

1.000

0.962

44.830

0.266

0.889

0.01925 -0.121

0.389

0.961

1.000

0.963

46.203

0.266

0.950

0.02020 -0.122

0.382

0.962

1.000

0.963

47.026

0.266

1.010

0.02184 -0.123

0.372

0.962

1.000

0.963

46.244

0.266

1.070

0.02113 -0.124

0.361

0.961

1.000

0.962

50.614

0.376

1.065

0.02310 -0.130

0.348

0.961

0.920

0.962

46.101

0.433

1.114

0.02396 -0.132

0.334

0.962

0.909

0.963

46.477

0.296

1.162

0.02500 -0.135

0.318

0.962

0.899

0.963

46.464

0.298

1.210

0.02633 -0.137

0.299

0.961

0.889

0.962

45.942

0.301

1.256

0.02774 -0.139

0.277

0.961

0.878

0.963

45.261

0.306

7.5 0.359 8.0 0.356 8.5 0.356 9.0 0.357 9.5 0.358 10.0 0.360 10.5 0.367 11.0 0.397 11.5 0.395 12.0 0.394 12.5 0.393 13.0 0.393 13.5 0.394 14.0 0.394 14.5 0.396 15.0 0.397

1.301

0.02921 -0.142

0.250

0.963

0.868

0.964

44.531

0.296

1.352

0.03457 -0.144

0.040

0.961

0.867

0.963

39.116

0.314

1.387

0.03684 -0.147

0.020

0.962

0.847

0.962

37.640

0.365

1.417

0.03893 -0.151

0.015

0.962

0.825

0.962

36.407

0.392

1.444

0.04097 -0.156

0.012

0.963

0.801

0.964

35.246

0.454

1.463

0.04422 -0.161

0.010

0.962

0.770

0.963

33.084

8.202

1.446

0.04870 -0.169

0.009

0.962

0.696

0.963

29.691

0.118

1.268

0.07186 -0.186

0.008

0.962

0.031

0.963

17.648

0.109

1.306

0.07523 -0.189

0.006

0.963

0.020

0.964

17.362

0.334

1.336

0.07909 -0.192

0.006

0.963

0.016

0.964

16.894

0.359

1.361

0.08293 -0.195

0.005

0.963

0.013

0.965

16.414

0.380

1.383

0.08735 -0.198

0.005

0.964

0.011

0.965

15.835

0.409

1.400

0.09569 -0.201

0.005

0.964

0.010

0.965

14.632

0.443

1.415

0.09937 -0.204

0.004

0.964

0.009

0.965

14.244

0.489

1.426

0.10879 -0.208

0.004

0.964

0.009

0.965

13.111

0.538

1.437

0.11696 -0.211

0.004

0.964

0.007

0.965

12.286

0.534

Name = naca-4412 Mach = 0; Re = 100000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition und effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. C.P. [?] [-] [-] [-] [-] [-] [-] -15.0 -0.519 0.12294 -0.027 0.922 0.005 0.198 -14.5 -0.498 0.12699 -0.030 0.915 0.005 0.191 -14.0 -0.476 0.11522 -0.032 0.910 0.006 0.182 -13.5 -0.453 0.10490 -0.035 0.904 0.006 0.173 -13.0 -0.427 0.09812 -0.038 0.899 0.006 0.161 -12.5 -0.399 0.09527 -0.041 0.893 0.006 0.148 -12.0 -0.370 0.08651 -0.043 0.889 0.007 0.132 -11.5 -0.338 0.08141 -0.046 0.880 0.007 0.113 -11.0 -0.305 0.07755 -0.049 0.871 0.008 0.089 -10.5 -0.270 0.07142 -0.052 0.862 0.008

model = 1; Aspect Ratio = 0; gro S.U.

S.L.

L/D

A.C.

[-]

[-]

[-]

[-]

1.000

0.009

-4.218

0.383

1.000

0.009

-3.924

0.377

1.000

0.010

-4.131

0.371

1.000

0.009

-4.315

0.364

1.000

0.009

-4.351

0.353

1.000

0.010

-4.186

0.348

1.000

0.010

-4.272

0.342

1.000

0.011

-4.149

0.336

1.000

0.012

-3.927

0.335

1.000

0.012

-3.787

0.332

0.058 -10.0 0.017 -9.5 -0.043 -9.0 -0.130 -8.5 -0.275 -8.0 -0.570 -7.5 -1.451 -7.0 0.050 -6.5 -0.007 -6.0 -0.097 -5.5 -0.263 -5.0 -0.669 -4.5 -6.247 -4.0 3.106 -3.5 1.345 -3.0 0.932 -2.5 0.748 -2.0 0.644 -1.5 0.577 -1.0 0.530 -0.5 0.496 0.0 0.470 0.5 0.449 1.0 0.431 1.5 0.417 2.0 0.405 2.5 0.395 3.0 0.386 3.5 0.379 4.0 0.372 4.5

-0.235

0.06648 -0.055

0.854

0.008

1.000

0.013

-3.532

0.328

-0.197

0.06341 -0.058

0.846

0.009

1.000

0.014

-3.108

0.326

-0.160

0.05863 -0.061

0.833

0.009

1.000

0.015

-2.721

0.326

-0.121

0.05425 -0.063

0.823

0.010

1.000

0.016

-2.227

0.324

-0.081

0.05091 -0.066

0.814

0.011

1.000

0.018

-1.589

0.323

-0.041

0.04788 -0.069

0.801

0.012

1.000

0.020

-0.851

0.229

-0.361

0.04513 -0.072

0.788

0.013

1.000

0.023

-7.994

0.227

-0.293

0.04149 -0.075

0.777

0.014

1.000

0.026

-7.057

0.293

-0.225

0.03893 -0.078

0.761

0.015

1.000

0.032

-5.780

0.293

-0.158

0.03726 -0.081

0.746

0.017

1.000

0.041

-4.232

0.291

-0.091

0.03473 -0.084

0.730

0.019

1.000

0.066

-2.620

0.423

-0.016

0.01725 -0.105

0.713

0.023

1.000

0.965

-0.941

0.430

0.037

0.01634 -0.107

0.693

0.028

1.000

0.967

2.286

0.270

0.098

0.01590 -0.108

0.674

0.034

1.000

0.968

6.192

0.268

0.160

0.01691 -0.109

0.652

0.043

1.000

0.968

9.438

0.268

0.221

0.01655 -0.110

0.629

0.058

1.000

0.968

13.340

0.268

0.282

0.01611 -0.111

0.603

0.084

1.000

0.969

17.503

0.268

0.343

0.01557 -0.112

0.574

0.120

1.000

0.970

22.028

0.268

0.404

0.01566 -0.113

0.541

0.170

1.000

0.970

25.800

0.268

0.465

0.01629 -0.114

0.502

0.249

1.000

0.970

28.537

0.268

0.526

0.01559 -0.116

0.459

0.881

1.000

0.963

33.715

0.267

0.586

0.01580 -0.116

0.431

0.912

1.000

0.962

37.118

0.265

0.647

0.01672 -0.117

0.417

0.940

1.000

0.962

38.698

0.266

0.708

0.01699 -0.118

0.407

0.961

1.000

0.962

41.656

0.266

0.769

0.01605 -0.119

0.401

0.961

1.000

0.962

47.882

0.266

0.829

0.01658 -0.120

0.395

0.961

1.000

0.962

50.009

0.266

0.889

0.01725 -0.121

0.389

0.961

1.000

0.963

51.560

0.266

0.950

0.01762 -0.122

0.382

0.962

1.000

0.963

53.889

0.266

1.010

0.01859 -0.123

0.372

0.962

1.000

0.963

54.338

0.266

1.070

0.01927 -0.124

0.361

0.961

1.000

0.962

55.503

0.267

0.366 5.0 0.361 5.5 0.356 6.0 0.352 6.5 0.359 7.0 0.357 7.5 0.355 8.0 0.354 8.5 0.354 9.0 0.355 9.5 0.355 10.0 0.356 10.5 0.359 11.0 0.363 11.5 0.398 12.0 0.395 12.5 0.394 13.0 0.394 13.5 0.394 14.0 0.395 14.5 0.396 15.0 0.397

1.129

0.01989 -0.125

0.348

0.961

1.000

0.962

56.772

0.267

1.188

0.02076 -0.126

0.334

0.962

1.000

0.963

57.209

0.267

1.246

0.02271 -0.127

0.318

0.962

1.000

0.963

54.872

0.431

1.235

0.02340 -0.135

0.299

0.961

0.920

0.962

52.746

0.528

1.281

0.02459 -0.137

0.277

0.961

0.909

0.963

52.117

0.301

1.327

0.02587 -0.139

0.250

0.963

0.900

0.964

51.318

0.311

1.368

0.03188 -0.142

0.040

0.961

0.886

0.963

42.910

0.341

1.401

0.03396 -0.146

0.020

0.962

0.863

0.962

41.244

0.367

1.432

0.03604 -0.150

0.015

0.962

0.843

0.962

39.745

0.376

1.462

0.03800 -0.154

0.012

0.963

0.822

0.964

38.464

0.410

1.485

0.04077 -0.158

0.010

0.962

0.796

0.963

36.432

0.490

1.502

0.04382 -0.163

0.009

0.962

0.765

0.963

34.277

0.768

1.507

0.04708 -0.170

0.008

0.962

0.723

0.963

32.023

0.126

1.286

0.07442 -0.190

0.006

0.963

0.043

0.964

17.278

0.124

1.327

0.07651 -0.192

0.006

0.963

0.023

0.964

17.347

0.325

1.356

0.08062 -0.195

0.005

0.963

0.017

0.965

16.817

0.363

1.379

0.08518 -0.198

0.005

0.964

0.013

0.965

16.191

0.395

1.398

0.09004 -0.201

0.005

0.964

0.012

0.965

15.523

0.433

1.413

0.09483 -0.204

0.004

0.964

0.011

0.965

14.898

0.483

1.424

0.09939 -0.208

0.004

0.964

0.010

0.965

14.332

0.526

1.435

0.10849 -0.211

0.004

0.964

0.008

0.965

13.230

0.533