An experimental study of the aerodynamics of a NACA 0012 airfoil with a simulated glaze ice accretion

APPENDIX A RUN SUMMARIES NACA 0012 MDEEL NO. 1 - GLAZE ICE CO_IGURATION SPLIT FILM VELOCITY PROFILES

x/c U-minE 6 IC O Ic Y-STAGIC Y-SEPIC

(c_g_) x10-6 (ft/s) (ft/s) xl03 xl03 236 -0.15 0.00 1.46 131.7 171.7 0.02146 0.42626 0.014721 0.020143 238 -0.15 -0.02 1.46 131.7 166.9 0.00950 0.35212 0.006662 0.008399 239 -0.15 0.02 1.46 131.7 170.0 0.02144 1.07510 0.012993 0.018715 240 -0.15 0.04 1.46 131.7 167.4 0.01697 0.77877 0.008640 0.014875 241 -0.15 0.06 1.42 133.5 176.1 0.01214 1.79805 0.004461 0.008394 242 -0.15 0.08 1.42 133.5 169.2 0.00737 3.05670 ....

243 -0.15 0.10 1.44 132.7 160.6 0.00489 2.90518 ....

244 -0.15 0.12 1.44 132.7 160.7 0.00375 2.56528 -- -- 245 1.85 -0.02 1.44 132.7 184.2 0.01161 0.21754 0.008947 0.010372 246 1.85 0.00 1.44 132.7 200.5 0.01265 -0.17896 0.020703 0.025558 247 1.85 0.02 1.44 132.7 201.7 0.03009 0.46930 0.021808 0.028466 248 1.85 0.04 1.44 132.7 201.8 0.02606 0.91716 0.016222 0.023689 249 1.85 0.06 1.44 132.9 199.4 0.02066 1.88002 0.009068 0.016413 250 1.85 0.08 1.44 132.5 191.8 0.01703 2.68549 0.006024 0.011304 251 1.85 0.10 1.44 132.5 185.3 0.01478 3.49155 0.004404 0.006891 252 1.85 0.12 1.44 132.5 176.7 0.01116 4.33792 ....

254 1.85 0.14 1.51 130.0 167.3 0.00835 4.28289 -- -- 255 1.85 0.16 1.51 130.0 165.5 0.00704 4.42153 ....

257 3.85 -0.02 1.51 130.0 180.0 0.01041 0.27493 0.008068 0.009076 258 3.85 0.00 1.51 130.0 202.4 0.02907 0.14864 0.022242 0.027926 262 3.85 0.02 1.54 129.0 200.0 0.03682 0.57272 -- 263 3.85 0.04 1.53 129.3 197.9 0.03195 1.15141 0.019096 0.029356 264 3.85 0.06 1.53 129.3 197.6 0.03110 1.91804 0.018119 0.027221 265 3.85 0.08 1.53 129.3 198.2 0.02875 2.72787 0.012555 0.022697 267 3.85 0.i0 1.49130.6 212.3 0.02849 3.10515 0.012515 0.021727 268 3.85 0.12 1.49 130.6 208.9 0.02717 3.90636 0.009639 0.018506 269 3.85 0.14 1.49 130.6 205.6 0.02418 4.80094 0.007583 0.012813 270 3.85 0.16 1.49 130.6 197.4 0.02072 5.57149 0.002420 0.004897 271 3.85 0.18 1.49 130.6 192.9 0.01939 6.21330 -- -- 272 3.85 0.20 1.49 130.6 186.8 0.01797 6.96573 ....

273 3.85 0.22 1.49 130.6 183.3 0.01687 7.44755 ....

274 3.85 0.30 1.49 130.6 175.4 0.01279 7.94107 -- -- 275 3.85 0.40 1.49 130.6 169.5 0.01223 8.40160 ....

276 3.85 0.50 1.49 130.6 166.5 0.01297 9.47147 ....

NACA 0012 MODEL NO. 2 - CLEAN OONFIGURATION Re xl0 -6 RUN CLu CL CD u CD CM u CM MACH ALPHA u ALPHA deg_> deg_!

0.0004 0.0003 0.126 1.465 -0.005 -0.005 0.0080 0.0078 364 0.00 0.00 0.0006 0.0005 0.126 1.484 -0.003 -0.003 0.0078 0.0076 365 0.00 0.00 0.0010 0.0017 0.126 1.484 0.i01 0.096 0.0080 0.0078 366 1.00 1.03 0.0010 0.0025 0.126 1.489 0.208 0.198 0.0083 0.0081 367 2.00 2.06 0.0011 0.0034 0.126 1.506 0.318 0.303 0.0085 0.0083 368 3.00 3.09 0.0023 0.0053 0.126 1.507 0.434 0.414 0.0092 0.0090 369 4.00 4.12 0.0027 0.0065 0.126 1.499 0.535 0.511 0.0095 0.0093 370 5.00 5.15 0.0010 0.0056 0.126 1.500 0.652 0.622 0.0098 0.0096 371 6.00 6.18 -0.0014 0.0041 0.126 1.499 0.774 0.738 0.0101 0.0099 372 7.00 7.21 0.0004 0.0066 0.126 1.500 0.870 0.829 0.0114 0.0111 373 8.00 8.24 0.0036 0.0105 0.126 1.501 0.962 0.917 0.0127 0.0124 374 9.00 9.27 0.0058 0.0132 0.125 1.493 1.052 1.003 0.0142 0.0139 375 10.00 10.29 0.0088 0.0168 0.126 1.497 1.134 1.080 0.0165 0.0161 376 ii.00 11.32 0.0127 0.0212 0.125 1.494 1.217 1.159 0.0205 0.0200 377 12.00 12.35 0.0152 0.0240 0.125 1.494 1.279 1.216 0.0261 0.0254 378 13.00 13.37 -0.1319 -0.1228 0.118 1.407 0.908 0.862 0.0317 0.0308 379 14.00 14.10 -0.1310 -0.1220 0.117 1.388 0.876 0.831 0.0373 0.0362 380 15.00 15.10 -0.0959 -0.0887 0.117 1.394 0.713 0.676 0.0429 0.0416 381 16.00 16.09 0.0146 0.0233 0.126 1.500 1.256 1.194 0.0233 0.0227 382 12.50 12.86 0.0179 0.0268 0.126 1.497 1.298 1.234 0.0289 0.0281 384 13.50 13.87 0.0021 0.0051 0.126 1.469 0.423 0.403 0.0092 0.0090 385 4.00 4.12 0.0004 0.0004 0.125 1.455 -0.007 -0.006 0.0072 0.0070 386 0.00 0.00 -0.0005 -0.0021 0.126 1.463 -0.228 -0.217 0.0078 0.0076 387 -2.00 -2.06 -0.0037 -0.0067 0.125 1.452 -0.437 -0.417 0.0075 0.0073 388 -4.00 -4.12 0.0011 -0.0038 0.125 1.459 -0.681 -0.650 0.0067 0.0065 389 -6.00 -6.18 0.0009 -0.0055 0.126 1.469 -0.900 -0.857 0.0127 0.0124 390 -8.00 -8.24 0.0010 -0.0039 0.126 1.462 -0.683 -0.651 0.0069 0.0067 391 -6.00 -6.19 -0.0031 -0.0070 0.125 1.455 -0.563 -0.537 0.0077 0.0075 392 -5.00 -5.16 -0.0061 -0.0137 0.127 1.478 -1.084 -1.032 0.0170 0.0166 393 -I0.00 -10.30 -0.0063 -0.0139 0.125 1.458 -1.077 -1.025 0.0170 0.0166 394 -10.00 -10.30 -0.0114 -0.0200 0.125 1.458 -1.240 -1.178 0.0272 0.0265 395 -12.00 -12.35 0.1055 0.0960 0.116 1.353 -1.015 -0.963 0.0374 0.0363 396 -14.00 -14.16 0.1087 0.0987 0.115 1.333 -1.057 -1.002 0.0425 0.0412 397 -15.00 -15.17 -0.0159 -0.0248 0.125 1.455 -1.299 -1.233 0.0323 0.0314 398 -13.00 -13.37 -0.0445 -0.0520 0.117 1.360 -1.191 -1.129 0.0349 0.0339 399 -13.50 -13.87 0.0003 0.0002 0.168 2.018 -0.015 -0.014 0.0087 0.0085 400 0.00 0.00 0.0002 0.0008 0.168 2.025 0.097 0.093 0.0081 0.0079 401 1.00 1.03 0.0006 0.0020 0.168 2.017 0.203 0.194 0.0083 0.0081 402 2.00 2.06 0.0002 0.0024 0.168 2.022 0.301 0.287 0.0086 0.0084 403 3.00 3.08 0.0008 0.0037 0.168 2.016 0.407 0.388 0.0087 0.0085 404 4.00 4.11 0.0017 0.0054 0.167 2.011 0.523 0.499 0.0098 0.0096 405 5.00 5.14 0.0004 0.0048 0.168 2.016 0.622 0.594 0.0099 0.0097 406 6.00 6.17 -0.0009 0.0045 0.167 2.009 0.742 0.708 0.0099 0.0097 407 7.00 7.20 -0.0010 0.0044 0.166 1.964 0.744 0.710 0.0089 0.0087 408 7.00 7.20 0.0012 0.0050 0.166 1.964 0.523 0.499 0.0087 0.0085 409 5.00 5.14 0.0001 0.0023 0.165 1.955 0.300 0.286 0.0083 0.0081 410 3.00 3.08 0.0004 0.0004 0.167 1.980 -0.004 -0.004 0.0076 0.0074 412 0.00 0.00 0.0001 0.0062 0.166 1.959 0.843 0.803 0.0112 0.0109 413 8.00 8.23 CD CM u CM MACH Re xl0 -6 CL u CL CD u 414 -2.00 -2.06 -0.224 -0.213 0.0071 0.0069 0.0000 -0.0016 0.167 1.970 415 -2.00 -2.06 -0.222 -0.212 0.0076 0.0074 0.0000 -0.0016 0.166 1.960 416 -4.00 -4.12 -0.420 -0.401 0.0082 0.0080 -0.0014 -0.0044 0.167 1.970 417 -6.00 -6.18 -0.646 -0.616 0.0085 0.0083 -0.0015 -0.0061 0.168 1.981 418 -8.00 -8.24 -0.868 -0.827 0.0114 0.0111 0.0003 -0.0059 0.167 1.974 420 9.00 9.26 0.929 0.886 0.0119 0.0116 0.0023 0.0089 0.165 1.948 421 i0.00 10.28 1.014 0.967 0.0140 0.0137 0.0048 0.0120 0.165 1.948 422 Ii.00 11.31 1.098 1.046 0.0158 0.0154 0.0069 0.0146 0.164 1.942 423 12.00 12.33 1.184 1.127 0.0184 0.0179 0.0093 0.0176 0.164 1.940 425 13.00 13.36 1.254 1.193 0.0220 0.0214 0.0116 0.0204 0.163 1.935 426 14.00 14.15 0.965 0.917 0.0256 0.0249 -0.1052 -0.0963 0.148 1.749 427 13.50 13.68 1.034 0.983 0.0238 0.0232 -0.0942 -0.0850 0.151 1.788 428 -i0.00 -10.29 -1.035 -0.986 0.0165 0.0161 -0.0040 -0.0113 0.166 1.958 429 -10.00 -10.29 -1.034 -0.985 0.0165 0.0161 -0.0036 -0.0109 0.166 1.960 430 -12.00 -12.34 -1.201 -1.142 0.0227 0.0221 -0.0100 -0.0183 0.166 1.957 431 -14.00 -14.20 -i.Ii0 -1.054 0.0289 0.0281 0.0919 0.0822 0.153 1.800 432 -13.00 -13.36 -1.267 -1.205 0.0258 0.0251 -0.0120 -0.0208 0.166 1.955 433 -13.50 -13.87 -1.292 -1.228 0.0274 0.0267 -0.0129 -0.0218 0.165 1.951 NACA 0012 MDDEL NO. 2 - ICED OONFIGURATION Re xlO -6 MACH RUN ALPHA u ALPHA CL u CL CD u CD CM u CM 434 0.00 -0.02 -0.039 -0.037 0.0282 0.0274 -0.0106 -0.0106 0.127 1.476 435 4.00 4.12 0.381 0.361 0.0399 0.0387 0.0134 0.0158 0.127 1.467 436 4.00 4.12 0.385 0.364 0.0401 0.0389 0.0140 0.0164 0.123 1.421 437 4.00 4.12 0.380 0.361 0.0401 0.0389 0.0147 0.0171 0.123 1.420 438 4.00 4.12 0.380 0.361 0.0390 0.0379 0.0135 0.0159 0.123 1.421 439 0.00 -0.02 -0.043 -0.041 0.0258 0.0251 -0.0103 -0.0104 0.124 1.428 440 1.00 1.01 0.070 0.066 0.0261 0.0254 -0.0056 -0.0050 0.124 1.429 441 2.00 2.05 0.176 0.167 0.0283 0.0275 0.0007 0.0019 0.124 1.426 442 3.00 3.08 0.274 0.260 0.0333 0.0324 0.0066 0.0084 0.124 1.457 443 4.00 4.12 0.380 0.360 0.0405 0.0393 0.0144 0.0167 0.123 1.455 444 5.00 5.15 0.478 0.452 0.0537 0.0520 0.0177 0.0207 0.123 1.452 445 6.00 6.16 0.553 0.521 0.0763 0.0735 0.0075 0.0112 0.122 1.443 446 7.00 7.14 0.601 0.561 0.1141 0.1092 -0.0252 -0.0201 0.121 1.431 447 8.00 8.10 0.577 0.535 0.1519 0.1442 -0.0549 -0.0485 0.121 1.438 448 9.00 9.07 0.521 0.479 0.1897 0.1787 -0.0704 -0.0633 0.120 1.429 449 0.00 -0.02 -0.038 -0.036 0.0270 0.0263 -0.0095 -0.0096 0.124 1.483 450 -2.00 -2.09 -0.251 -0.238 0.0345 0.0335 -0.0172 -0.0187 0.124 1.482 451 -4.00 -4.14 -0.444 -0.420 0.0494 0.0479 -0.0194 -0.0220 0.123 1.477 452 -4.00 -4.14 -0.443 -0.420 0.0503 0.0487 -0.0203 -0.0230 0.123 1.406 453 -6.00 -6.13 -0.577 -0.544 0.0649 0.0627 0.0218 0.0171 0.121 1.392 454 -8.00 -8.08 -0.516 -0.486 0.0798 0.0769 0.0553 0.0500 0.120 1.379 455 -7.00 -7.11 -0.547 -0.515 0.0724 0.0698 0.0332 0.0284 0.120 1.377 456 -6.00 -6.13 -0.580 -0.547 0.0649 0.0627 0.0232 0.0185 0.121 1.389 457 -5.00 -5.15 -0.536 -0.505 0.0686 0.0662 -0.0043 -0.0079 0.122 1.402 458 0.00 -0.02 -0.043 -0.041 0.0272 0.0265 -0.0101 -0.0102 0.161 1.883 459 2.00 2.05 0.167 0.159 0.0287 0.0279 0.0008 0.0020 0.161 1.880 460 4.00 4.11 0.364 0.345 0.0417 0.0405 0.0135 0.0158 0.160 1.870

CD u CD CM u CM MACHRe xl0 -6

ALPH_ u ALPHA CLu CL

1.840

0.0741 0.0052 0.0088 0.157

461 6.00 6.15 0.535 0.504 0.0769

0.154 1.798

0.1073 -0.0443 -0.0387

462 8.00 8.11 0.575 0.537 0.1121

0.155 1.815

0.0908 -0.0294 -0.0244

463 7.00 7.12 0.568 0.532 0.0945

0.152 1.775

0.1237 -0.0679 -0.0618

464 9.00 9.06 0.489 0.455 0.1297

0.160 1.875

0.0332 -0.0178 -0.0192

465 -2.00 -2.08 -0.238 -0.226 0.0342

0.161 1.904

0.0332 -0.0181 -0.0194

466 -2.00 -2.09 -0.239 -0.227 0.0342

0.160 1.890

0.0490 -0.0199 -0.0225

467 -4.00 -4.14 -0.424 -0.401 0.0506

1.858

0.157

0.0806 0.0038 -0.0002

468 -6.00 -6.15 -0.546 -0.513 0.0837

0.154 1.826

0.1117 0.0187 0.0135

469 -8.00 -8.16 -0.644 -0.601 0.1168

1.806

0.153

0.1271 0.0280 0.0221

470 -9.00 -9.16 -0.688 -0.640 0.1334

0.150 1.777

0.1424 0.0360 0.0294

471 -I0.00 -10.16 -0.729 -0.676 0.1499

0.152 1.794

0.1424 0.0549 0.0496

472 -I0.00 -10.05 -0.414 -0.384 0.1499

0.153 1.814

0.1117 0.0491 0.0435

473 -8.00 -8.10 -0.545 -0.508 0.1168

0.157 1.859

0.0865 0.0144 0.0101

474 -6.00 -6.13 -0.537 -0.504 0.0900

0.160 1.894

0.0490 -0.0185 -0.0211

475 -4.00 -4.14 -0.426 -0.403 0.0506

1.840

0.156

0.0909 0.0261 0.0211

476 -7.00 -7.13 -0.582 -0.546 0.0947

0.848

0.075

0.0243 -0.0104 -0.0106

477 0.00 -0.02 -0.048 -0.046 0.0250

0.075 0.853

0.0271 0.0002 0.0015

478 2.00 2.05 0.182 0.173 0.0278

0.849

0.075

0.0381 0.0143 0.0168

479 4.00 4.12 0.396 0.375 0.0392

0.844

0.074

0.0693 0.0122 0.0160

480 6.00 6.17 0.575 0.542 0.0718

0.830

0.073

0.I001 -0.0490 -0.0432

481 8.00 8.11 0.596 0.558 0.1044

0.826

0.073

0.1156 -0.0735 -0.0668

482 9.00 9.08 0.571 0.533 0.1210

0.836

0.074

0.0846 -0.0243 -0.0192

483 7.00 7.14 0.624 0.586 0.0880

0.075 0.849

0.0294 -0.0187 -0.0203

484 -2.00 -2.09 -0.269 -0.256 0.0302

0.075 0.845

0.0462 -0.0208 -0.0237

485 -4.00 -4.15 -0.470 -0.445 0.0477

0.834

0.074

0.0807 0.0216 0.0167

486 -6.00 -6.14 -0.603 -0.566 0.0839

0.826

0.073

0.1001 0.0651 0.0592

487 -8.00 -8.07 -0.528 -0.494 0.1044

0.833

0.074

0.0846 0.0527 0.0470

488 -7.00 -7.10 -0.581 -0.546 0.0880

0.842

0.074

0.0646 -0.0094 -0.0132

489 -5.00 -5.17 -0.567 -0.535 0.0669

0.862

0.075

0.0243 -0.0105 -0.0107

490 0.00 -0.03 -0.050 -0.047 0.0250

0.861

0.075

0.0271 0.0011 0.0023

491 2.00 2.05 0.177 0.169 0.0278

0.857

0.074

0.0381 0.0143 0.0168

492 4.00 4.12 0.398 0.378 0.0392

0.851

0.074

0.0693 0.0117 0.0155

493 6.00 6.17 0.583 0.549 0.0718

0.074 0.856

0.0462 -0.0210 -0.0238

494 -4.00 -4.15 -0.469 -0.444 0.0477

0.861

0.075

0.0294 -0.0196 -0.0211

495 -2.00 -2.09 -0.258 -0.245 0.0302

0.872

0.075

0.0076 0.0006 0.0005

500 0.00 0.00 -0.011 -0.010 0.0078

0.873

0.075

0.0075 0.0013 0.0028

501 2.00 2.06 0.213 0.203 0.0077

0.875

0.076

0.0086 0.0030 0.0060

502 4.00 4.12 0.435 0.415 0.0088

0.876

0.076

0.0087 -0.0026 0.0024

503 6.00 6.19 0.691 0.659 0.0089

0.076 0.875

0.0126 0.0021 0.0084

504 8.00 8.24 0.888 0.846 0.0129

0.876

0.076

0.0161 0.0086 0.0160

505 i0.00 10.30 1.061 1.010 0.0165

0.076 0.876

0.0165 0.0092 0.0166

506 i0.00 10.30 1.061 1.010 0.0169

0.075 0.873

0.0238 0.0166 0.0247

507 12.00 12.34 1.189 1.131 0.0244

0.072 0.832

0.0310 -0.1027 -0.0946

508 14.00 14.12 0.842 0.800 0.0319

0.871

0.075

0.0274 0.0011 0.0094

509 13.00 13.32 1.166 1.108 0.0282

0.872

0.075

0.0256 0.0170 0.0251

510 12.50 12.84 1.188 1.129 0.0263

0.076 0.879

0.0080 -0.0010 -0.0026

511 -2.00 -2.06 -0.233 -0.222 0.0082

0.076 0.896

0.0098 -0.0035 -0.0067

512 -4.00 -4.13 -0.452 -0.431 0.0100

0.076 0.899

0.0134 0.0061 0.0009

513 -6.00 -6.19 -0.714 -0.681 0.0137

0.895

0.076

0.0130 0.0060 0.0008

514 -6.00 -6.19 -0.710 -0.677 0.0133

CD CM u CM MACHPe xl0 -6

BEN ALPHA u ALPHA CL u CL CD u 515 4.00 4.12 0.433 0.413 0.0080 0.0078 0.0024 0.0055 0.076 0.901 516 -8.00 -8.25 -0.909 -0.866 0.0146 0.0142 -0.0029 -0.0093 0.076 0.900 517 -10.00 -10.31 -1.093 -1.040 0.0192 0.0187 -0.0097 -0.0173 0.076 0.902 518 -12.00 -12.35 -1.210 -1.150 0.0269 0.0262 -0.0163 -0.0246 0.076 0.894 519 -14.00 -14.12 -0.847 -0.804 0.0346 0.0336 0.1031 0.0949 0.073 0.858 520 -13.00 -13.32 -1.164 -1.105 0.0308 0.0300 0.0005 -0.0078 0.076 0.895 521 -12.50 -12.85 -1.197 -1.138 0.0288 0.0280 -0.0191 -0.0272 0.076 0.900 NACA 0012 MODEL NO. 2 - CLEAN CONFIGURATION TRIP AT X/C = 0.05 (BOTH UPPER AND LOWER SURFACES) Re xl0 -6 MACE

ALPHA u ALPHA CLu CL CDu cD c% cM

748 0.00 0.00 -0.006 -0.006 0.0081 0.0079 -0.0025 -0.0025 0.116 1.387 749 8.00 8.25 0.875 0.832 0.0108 0.0105 -0.0015 0.0051 0.116 1.386 750 8.00 8.25 0.880 0.837 0.0111 0.0108 -0.0025 0.0042 0.116 1.387 751 0.00 0.00 -0.006 -0.006 0.0109 0.0106 -0.0001 -0.0002 0.116 1.374 * 752 2.00 2.06 0.217 0.207 0.0111 0.0108 0.0007 0.0023 0.117 1.384 * 753 4.00 4.13 0.438 0.417 0.0115 0.0112 0.0004 0.0037 0.116 1.380 * 754 2.00 2.06 0.208 0.198 0.0110 0.0107 -0.0013 0.0003 0.117 1.385 * 755 4.00 4.12 0.430 0.409 0.0116 0.0113 -0.0012 0.0021 0.117 1.391 * 756 6.00 6.19 0.653 0.620 0.0136 0.0133 0.0006 0.0055 0.116 1.381 * 757 8.00 8.25 0.849 0.806 0.0139 0.0135 0.0045 0.0109 0.117 1.390 * 758 10.00 10.31 1.038 0.986 0.0176 0.0171 0.0083 0.0161 0.115 1.370 * 759 12.00 12.36 1.198 1.136 0.0247 0.0240 0.0139 0.0226 0.116 1.373 760 14.00 14.13 0.932 0.882 0.0318 0.0309 -0.1248 -0.1151 0.109 1.293 761 13.00 13.38 1.247 1.181 0.0299 0.0290 0.0167 0.0257 0.116 1.375 762 -4.00 -4.14 -0.463 -0.440 0.0125 0.0122 -0.0030 -0.0065 0.117 1.394 763 -8.00 -8.26 -0.856 -0.812 0.0173 0.0168 -0.0055 -0.0119 0.116 1.380 764 -13.00 -13.37 -1.190 -1.127 0.0283 0.0275 -0.0184 -0.0270 0.109 1.295 765 -14.00 -14.19 -0.939 -0.889 0.0318 0.0309 0.0728 0.0641 0.113 1.337 766 -12.00 -12.36 -1.174 -1.112 0.0285 0.0277 -0.0160 -0.0246 0.116 1.376 * NOTE: Pressure difference between transducers.

NACA 0012 MODEL hD. 2 - CLEAN CONFIGURATION TRIP AT X/C = 0.05 TOTAL BOUNDARY LAYER PROBE VELOCITY PROFILES

e/c

RUN AOA X/C Re VEL U-EDGE 6 /C xl03 (deg) x10-6 (ft/s) (ft/s) xl03 2.10189 788 3.85 0.03 1.43 131.8 151.8 3.20166 2.10328 789 3.85 0.03 1.41 130.7 151.1 3.21301 1.42940 790 3.85 0.02 1.42 131.6 163.9 2.15226 1.50410 791 3.85 0.02 1.42 131.1 163.3 2.33087 1.57792 792 3.85 0.02 1.42 131.3 162.9 2.37040 1.79168 793 3.85 0.02 1.41 130.8 162.8 2.76799 0.93361 794 3.85 0.01 1.42 131.2 162.7 1.53397 1.02513 795 3.85 0.01 1.42 131.0 163.9 1.69846 0.43989 796 3.85 0.00 1.42 131.3 194.0 0.77307 0.55715 797 3.85 0.00 1.43 132.5 194.8 0.88946 1.57829 798 -0.15 0.03 1.43 131.1 148.0 2.30661 1.52718 799 -0.15 0.03 1.43 132.4 147.9 2.28867 1.03879 801 -0.15 0.02 1.44 132.0 155.8 1.58051 1.17000 802 -0.15 0.02 1.43 130.4 155.5 1.80664 0.67952 803 -0.15 0.01 1.44 131.8 159.4 1.10019 0.77926 804 -0.15 0.01 1.44 131.6 159.4 1.24502 0.24111 805 -0.15 0.00 1.44 131.5 159.2 0.53174 0.33051 807 -0.15 0.00 1.44 131.6 159.8 0.62718 0.65278 808 -0.15 0.01 1.49 132.9 179.8 1.12362 1.12934 811 -0.15 0.02 1.48 132.8 168.2 1.72779 1.22531 812 -0.15 0.02 1.48 132.3 168.0 1.95480 1.74612 813 -0.15 0.03 1.48 132.2 155.4 2.63122

APPENDIX B PRESSUREDISTRIBUTIONS Pir_l_;_i_NG PAGE BLANK NOT FILMED RUN 0364 R0R -.00 In= M 0.13 RE 1.46 CL -.005 N.

CON 0.0078 CM 0.0003 IV.

O ii, eml I O Q.

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O. $0 O. 80 I . O0 X/c RUN 0365 ROR -.00 in, ' H 0.13 1.48 RE -.003 CL !

0.0076 CDN 0.0005 CI'I

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==

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O =A I _ I O, 80 t. O0 "0 O0 O. 20 O. 40 O. 80

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RUN 0366

==

_ ROR 1.03 I

H 0.13

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==

CL 0,096

('ql,

COg O. 0078

CH 0.0017

==

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RUN 0367 ROR 2.06 ano M 0.13 RE 1.49 o M1 CL 0.198 I CON 0.0081 CM 0.0025 o M1 I OI & VVVW_Vv v vV v V & &A IIII.

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==

ROR 4.12 Irt° M 0.13 RE 1.51 a CL 0.414 I COH O. OO90 CM 0.0053

==

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O g- Q o z II I • I O. 20 O. 40 O. 60 0 • 80 I • O0 "o O0 X/C

RUN 0370

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==

0.511

CL

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0.0093

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R0R 7.21 i M 0.13 RE 1.50

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COH 0.0099 CM 0.0041

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CL 1.234 CON 0. 0281 CM 0.0268 OI

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RUN 0391 ==.

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RUN 0395 g ROR -12.35 I H 0.13 RE 1.46 CL -1.178 CON 0.0265 CH -.0200 V (jI V e !

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O O ItS

ROR 13.38

4=,l I

M 0.12

RE 1.37

CL 1. 181

e,,,e a

COW O. 0290

CM 0.0257

==

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o A

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Oq ¢} I g g g g 0.20 0.40 0.60 0.80 I . O0

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ROR -4. t4 PI O. t2 RE 1,39 o CL -.440 I%1, CON O. 0 t 22 CH -.0065

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RUN FIOR -8.26 Yr.

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COW 0.0168 CM -.0119 0_ '9.

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CON 0.0275 CH -.0270 ¢D O qlzq !

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RUN 0365

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POSITION JN HAKE (IN)

RUN 0367

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_a • -i, o I,,,,4 g,e (/')

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POSITION ,IN HAKE (IN)

RUN 0369

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POSITION IN NRKE (IN)

RUN 0371

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AOA 6.18

HACH O. 1::)

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go z"oo "1: oo e"oo s'.eo z'e.eo

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(IN)

RUN 0373

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t,.ql_ w (/1 U.I u./al IL/ li= m G: _r ,11.

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RUN 0375

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POSITJON JN HFiKE (IN)

RUN 0377

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RUN 0439

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POSITION IN PlFIKE (]Hi

RUN 0377

CD O, 0200

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.-"a 11'_8 wO w IcJ Q'm (Z Z

POSITION IN MAKE (IN)

RUN 0441

CD 0.0275

AOA 2.05

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,...bo ii-_ g.e W (f) UJ _l'JO O'J iY" =e Im "m .W

RUN 0443

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POSITION IN HAKE (IN)

RUN 0450

CD O. 0335

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POSITION IN HI:iKE (IN)

RUN 0451

CD 0.0479

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1'-41,4 I_'1°

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POSITION IN HRKE (IN)

RUN 075[

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RSR 0.00

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RUN

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%' POS]TJON JN HRKE (JN) .oo

RUN 0753

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RUN

CD

0.0133

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6.19

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0.12

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POSITION IN HI:IKE (IN)

RUN 0757

CO 0.0135

ROR 8.25

MRCI:I O. 12

N

,.-b o i..-i g.e W (3") Q,) IL m m I, D N II O0 2. • O0

POSITION IN WAKE (IN}

RUN 0758

CD 0.0171

ROll 10.31

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POSITION IN HllKE (IN)

RUN 0759

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ROR 12.36

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POSITION IN HRKE (IN)

RUN 0761

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APPENDIX D VELOCITY PROFILES o NRCR 0012 M]TH GLRZE ]CE "1 UPPER SURFRCE RUN 236 o ROR -.15 ql" X/C -.00 VEL 131.7 RE 1.46 O O m Oi Z N w O >-N el Q IO ,=;- o (D Q ql,

Q

f

!

II =;-4o. oo

a.o0 46.0o eb.0o z _0.0o

] 60. O0 200.00 240, O0 U (FT/SEC) o NRCR 0012 WITH GLRZE ICE ml "1 UPPER SURFRCE (9 RUN 238 (9 ROR -.15 X/C -.02 VEL 131.7 RE 1.46 o o z w o >-1o

Q

o =;- ® o t_ 0 Q B !

°-40. oo o'. oo g'O. O0 1'20. O0

40.00 160.00 2bo. oo 2:_o.oo

U (FT/SEC} o GLRZE ICE =1 _;- NRCR 0012 WITH UPPER SURFRCE RUN 239 o ROR -. 1S ,it _;. X/C 0.02 VEL 131.7 RE 1.46 o o I0 J_ Z o e= Q

¢ 0 ®

= 0

_ •

| | -40. O0 O. O0 40.00 eo. oo 1_o. oo l_o. oo zoo. oo z_o. oo U (FT/SEC) o ,q, NRCR 0012 WITH GLRZE ICE -I "i UPPER SURFRCE RUN 240 o ROR -.IS ru X/C 0.04 VEL 131.7 RE 1.46 L--m

i

¢= o

=;-

i

Z =,,,-I w o >,.to

4"

II

o

@

qP om o t_ B ¢;.

Q | | II °-40. O0 0;00

40.00 eo.oo 1_o. oo 1_0.0o

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|

o ID 4" z w o

@

¢;-

Q (D(9 O =;- Olp == B =.J .

°-40.00 0.00

,:o.oo e'o.oo 1_o.0o 16o.oo abo.oo 2_o.oo

U (FT/$£C} o GLRZE ICE ml NRCR 0012 HJTH ,iPa UPPER SURFRCE RUN 242 ¢} ROR -.15 X/C 0.08 em YEL 133.5 RE 1.42 o ¢} e_ ,,me ¢0 ¢;- z w o >,._ Q

¢

® ® o (%1 G," (am)

#

B 'mr "r T Ir- T I 1 _o.oo 120.00 180,00 200. O0 240.00 200,00 40.00 80.00 U (FT/SEC) o NRCR 0012 WiTH GLRZE e. ICE ,1 UPPER SURFRCE RUN 243 ¢= ROR -.15 X/C 0.10 YEL 132.7 RE 1.44 o O ed ® o m c;" 7' w o

&

O qP O I%1 ® Q | ! | ;0.00 e'o.oo 1oo.oo 1;_o. oo 1,_o.oo ,eo.oo 1_o.oo zoo.oo U (FT/SEC) o ,qp GLRZE ICE =1 NRCR 0012 WITH UPPER SURFRCE RUN 244 ROR -.15 o I%1 X/C 0.12 ea e=,e VEL 132.7 RE 1.44 o o, o z w o >.,ID ¢;- (9 dl) ,=;- ® ® o I'M =;- o o ) o, I I I 166, O0 10s.0o l_,s. 0o zz6.00 {3s. 0o 14s.0o l'_s. 0o

%i

,00

U {FT/SEC}

O NRCR 0012 M]TH GLRZE ]CE =1 UPPER SURFRCE RUN 24S O ROR 1.8S N X/C -.02 o.

eml VEL 132.7 RE 1.44 Q o (= el ei i (=l

>._.-

o o qP Q oi

° 81

_40.00 0'.00

46.00 e6.00 1_0.00

lto.oo 2'00.00 2'40. 00"

U (FT/SEC} o qr GLRZE ICE =1 NRCR 0012 WITH UPPER SURFRCE

==

RUN 1.85 0 ROR N 0,00 X/C YEL 132.7 RE 1.44 (g & el O=a o o Q z I--,I 0 w o B >..to =;- Q @ (D ® P O ql" ¢;- =, o Q ¢;

L

1' T I T I 200. O0 240. O0 °-40.00 0.00 40. O0 80.00 120. O0 U (FT/SEC) O ql' NRCR 0012 WIIH GLRZE ICE -1 UPPER SURFRCE RUN 247 _P O ROR 1.85 I'M X/C 0.02 VEL 132.7 RE 1.44 e,_ o JI g Z h,q Q ® g) (9 _P o D Q Q _ N 0 Q o -40.00

o:oo 4b.oo sb.oo 1_o.oo l'eo. oo z'oo.oo 2_o.oo

U (FT/$EC} ¢} ql" NRCR 0012 _JTH GLflZE ICE ,,1 "a UPPER $URFRCE RUN 248 O ROR 1.8S N X/C 0.04 el VEL 132.7 RE 1.44 Q .i" O =;- z w o _ZD =;- o qP

,%

Q c;" ® Q o Q o ! Ir | I md O, O0 0'.00 40.00 !10. O0 1_0.00 lEiO. O0 200. O0 240.00 U (FT/SEC] qP NACR 0012 NITH GLRZE ICE UPPER SURFRCE RUN 249 O ROR 1.85 n,I X/C 0.06 YEL 132.9 RE 1.44 ¢D D ¢:) m

=;-

z

|

e

o >,.u_ Q ,It

,=;-

Q D I%1 Q =;- @ -_10. O0

o'.oo 4b.oo fo.oo l'zo.oo l'eo.oo zbo.oo

U (FT/SEC} o ,qr GLRZE ICE -,1 NRCR 0012 WITH el UPPER SURFRCE RUN 2S0 ROR 1.85 o Pd X/C 0.08 el • EL 132.5 RE 1.44 o ¢= el ® ® ¢= I0 ¢;-

i

z w o >,.u_ ¢;- o ,it qi_ ® Q _X9 dP Q N Q =;- (]o =.,p d.oo 4b.oo 86.00 1_o.oo lko.oo zbo.oo z4o.oo °-40. O0 U (FT/$EC) o qP NRCR 0012 WITH GLRZE ICE =1 UPPER SURFACE RUN 2S1 O ROR 1.85 t_ X/C 0.10 YEL 132.S

i

RE 1.44 ¢1

!

m

@

g) Z Q >-CO

@

=;- o _P Q ,=;-

lip

O O I f_J aid g) | I I o'.o0 4b.0o so.oo tzo.oo _so.oo zbo.00 2_o.oo U [FT/SEC] ¢) GLRZE ICE =l NRCR 0012 WITH "i UPPER $URFRCE RUN 252 ROR 1.85 o t%l X/C 0,12 el =me VEL 132,5 RE 1.44

!

e ¢) ¢) m ¢;- z O Q Q >.to Q O ¢= ,qp 6, (D ® o N

%8 ®Q

I I i I "" O0 _ 80. O0 120. O0 180. O0 Z()O. O0 240. O0 280. O0 o(_, 40°00 U (FI'/SEC) Q el NRCR 0012 M]TH GLRZE ICE al UPPER SURFRCE RUN 254 ¢D ROR 1.85 I'M Oi X/C 0.14 VEL 130.0

t

RE 1.51 O O O m Z w o o ml'

c;"

¢m O ® O ,=;- (D • o.J O ' 40. oo s6. oo

ob.oo 1'oo.oo l_o.oo 1:!o. oo sko.oo lbo.oo

U (FT/SEC) o qP NRCR 0012 HITH GLRZE ]CE =t UPPER SURFRCE RUN 255 o ROR 1.85 l%1 X/C 0.16 ® YEL 130.0 RE 1.51 o el z w o >.._ ,=;- o

R

v ¢;- o ® (P® =;- ® "l °80. O0 e6.oo lbo.0o lJ, o.oo 1_o.oo 1_o.oo 1%o.oo z oo.oo U (FT/SEC} o ql' o, NRCR 0012 MZTH GLRZE ICE ,,1 UPPER SURFRCE ® RUN 257 ROR 3.85

N |

Ba X/C -.02 VEL 130.0 RE 1.Sl Q ¢D

|

o.

¢) I0 h,q >..u_ o ql,'

l

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0.,, _,

°-4o.oo o.oo 4b.oo eb.oo iJ_o.oo ,ko.oo

2bo. oo

2_40, O0 U (FT/SEC) o IO ICE =I GLRZE NRCR 0012 MITH

&-

UPPER SURFRCE t RUN 258 ROR 3.8S o qP X/C 0.00 &.

VEL 130.0 RE 1.$1 C) o (: el Z

!

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¢) o.

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c;"

==

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C:D NRCR 0012 M]TH GLRZE ICE =1 `4- UPPER SURFRCE RUN 262 o ROR 3.05 ql' X/C 0.02 `4.

VEL 129.0 RE 1.54 O ,4" Q OI tml Am_ Q >..N I0 O =;- _m

B

Q 0@

4'

m qP o o le I | -, O. O0 O. O0 40. oo 8o. oo 1_o. oo t eo. oo zoo. oo z4o. oo U (F'r/SEC] o GLAZE NRCR 00t2 MITH ICE =1 el UPPER SURFACE RUN 263 ROR 3.85

|

N X/C 0.04 4l I VEL 129.3 RE 1.53 o

i

o ,I I o o Q O l0 ,=;- z I,,-,,l Q w O ¢= >,,_ ,=1- ql) ® O v 0® ,=;- o N e ,=;- B _P O o ,=; od O. O0 o;oo 4b.oo eS.oo z_.o.oo ndo.oo z6o.oo z:qo.oo U (FT/SEC) Q qP NACR 0012 HJTH GLAZE TCE -,1 UPPER SURFACE RUN 264

|

AOR 3.85 I%1 X/C 0.06 ¥EL 129.3 RE 1.53 O O ID am) (5 Z O o Q qP c;" II c;" o •

=. B

ii o-40, O0 | O. O0

46.00 eb.oo 1_o.oo lko.oo 2'oo.ao

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&-

UPPER SURFRCE RUN 265 AOR 3.85 O qP X/C 0.09

&-

YEL 129.3

RE 1.53

o

r;"

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,=;-

eQ

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==

om | o.,

eb.oo z_o.oo

O. O0 O. O0 40. O0 lifO. O0 2O0. O0 2_10. O0

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o g NRCR 0012 MITH GLRZE ICE =1 &.

UPPER SURFRCE RUN 267 0 ROR 3.85 qp X/C 0.10 &- VEL 130.6 RE 1.49 &- a Ip Bml tma Z w o _,,r_ ej

/

O ,rod c_" L,-U O

dm

e@

a qP c_" el I °-40. O0 O. O0

4b.oo e6.oo z_o.oo s'oo. oo z'oo. oo z:_o. oo

U {FT/SEC) o m GLRZE ]CE =t HRCR 0012 WITH UPPER SURFRCE RUN 268 ROR 3.85 o _/C 0.12 i, VEL 130.6 RE 1.49 m I o i i z o )-N o, fd m =;- ® o qP e4

,F D

dp ®P

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240, O0 4b.a0 e6.o0 j_0.0o l&o.0o z6o.o0 0. o0 _. oo U (FT/SEC) ID NRCR 0012 NITH GLRZE ICE =1 UPPER SURFRCE RUN 269 O ROR 3.85 qP X/C 0.14 YEL 130.6 RE 1.49 Q oll ¢lm Z 1,11 >-rV Q IB c;" edP

®'B

ee ql, • •

eo

c;"

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Q

aP

io.oo o:oo 4b. oo

8b.oo 1'2o.oo 3_o.oo 2bo.oo

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o e, wine w O >-N

t

e, l.e o qP

ee

o Q m(9 o.

I o _O. O0 4b.oo sb.oo 1'2o.oo {so. oo 2bo.oo 2_o. oo O. O0 U {FT/SEC} NRCR 0012 WITH GLRZE ICE al UPPER SURFRCE RUN 271 Q ROR 3.85 X/C 0.18 VEL 130.6 RE 1.49 Q ,4" I@ .m z I,.,,.I Q II e o I0 ,G" ,,,e,

mP

elQ el_ II % 4b lIO0 g Oh. O0 J_o.oo Ido.oo 200, O0 2_10.00 28O'. O0 U (PT/SEC) o m -1 NRCR 0012 WITH GLRZE ICE &- UPPER SURFRCE RUN 272 D AOR 3.85 ql' X/C 0.20 &- YEL 130.6 1.49 RE Q O ID o.

Z >-N • a Q m Q

@

O qlP oJ I II I _" oo 4o. oo sb.oo n2o.oo t_o.oo zoo.oo z4o. oa z_o. oo U (FT/SEC) O NACA 0012 H]TH GLAZE ]CE ml &- UPPER SURFRCE RUN 273 O ROR 3.e5 'ql" X/c 0.22 &- VEL 130.6 RE 1.49 Q &- tO I) I tree 6m_ Z_ I.m,I w >-ru el m_ tO c;"

eG )

o i ,qp ale o o e..

| F II

°o_ oo 46.00 1_,o.oo Iko.oo :,b0.o0

80.00 240. O0 2OO. OO U (FT/SEC) m RRCR 0012 HITH GLRZE ICE ml UPPER SURFRCE RUN 274 0 ROR 3.85 v X/C 0.30 _EL 130.6 RE 1.49 O W "i w ...;' O m c;" _. ®0 _p Q ¥

. 100"_. 0"_ ,20.0-_

140.00 180.00 200. DO" U {F'I'/SEC) ' 0 m NRCR 0012 WITH GLRZE ICE -t &- UPPER SURFRCE RUN 275 O ROR 3.85 ql' X/C 0.40 &- ¥EL 130.6 RE 1.49

t

B Z w Q oel eme m ,=;- ql.

c;" 1.00 8_.00 -0 1 r • 00 120.00 140.00 1_00. O0 U (FT/SEC) m NRCA 0012 HITH GLRZE ICE _1 &- UPPER SURFRCE RUN 276 ROR 3.85 ql" X/C 0.50 &- YEL 130.6 RE 1.49 O &- U_ e.

Z Iml w >.rv ol W &- qP &.

qpe

11 II 60. O0 80. O0 100. O0

z_o.oo z_o.oo zko.oo zko.oo ioo..oo

U (FT/SEC) o NRCR 0012 HOOEL el a2 MITH TRIP R'I' X/C-.OS UPPER SURFRCE RUN 78B 0 ROR 4.00 X/C 0.70 el VEL 131.8 RE 1.43 O o el ID ,=;- >,,, LO ,=;- o ql" ,=;- o N dp® _°

®,,s

o0 I. 00 sb. 00 _ e'o. oo 2bo.oo 2do. oo

2t0.00 z_0.0o

bo, oo

U {FT/SEC) ¢= -2 WIIH IRIP R'r X/C-.05 NRCR 0012 MODEL o== ewe UPPER SURFRCE ?89 RUN o 4.00 ROR N 0.?0 X/C YEL 130.?

RE 1.41 o ¢l Om f=O o qo ¢;- Z w o >,._ ¢;- ¢D ql" =;- o N ¢;- o o t I | I I I I I =, 1.00 60.00 80,00 100, O0 120,00 140,00 160, O0 100.00 U CFT/SEC) ID NRCR 0012 HODEL =2 MXTH TRIP RT X/C-.O5 =;- UPPER SURFRCE RUN 790 m qP X/C 0.S0 c;" ROR 4.00 YEL 131.6 RE 1.42 w,!

ql" =;- let c;"

i

Z w qP O >-N =;- I W (aB c;" ID eQ =;- BJ OI 60, O0 00. O0

lbo.oo 1_o.oo l;eo. oo lko.oo lbo. oo z'oo. oo

U {FT/SEC) =2 MJTH TRiP RT X/C-.05 NRCR 0012 NOOEL UPPER SURFRCE RUN 791 m 80R 4.0O ql, X/C 0.5O

I

VEL 131.1 RE 1.42 o ql,, F'I

!

z w >,, I_,l B= ,D O em ® 1' 1" 11" 1 I" I' 120. O0 140.00 180.00 IBO. O0 200.00 100. O0 80, O0 U {FT/SEC} Idea NFICFI 0012 MODEL "2 H,[TH TFI.[P FIT X/C-.O5 UPPER SURFFICE RUN 792 m FIOFI 4.00 X/C 0.50 VEL 131.3

|

RE 1.42 O ql'

c;" i

N M c;" ,el, c;" c;" Q m _ o Q cl_ ® eb.oo z6o.0o

1_,o. oo 1:_o. oo z ko.oo I iJo. oo abo. oo

U (FT/SEC) tO in RT X/C-.O_ ,,2 glTH TRIP NRCR 0012 NSOEL ,=;- UPPER SURFRCE RUN 794 tO RSR 4.00 ql'

!

_/C 0.30 ¥EL 131.2

|

RE 1.42 o ,i, ,=;-

!

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I

>.N @.

I Q tO I0 g) 200. O0

16o. oo 1_0.o0 z_0.o0 1'eo.0o z'eo.oa

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|

VEL 130.8 RE 1.41 qP

i

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II

z (9 e w

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