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HQ17 Airfoil

Airfoil measured from an ASW22 wing

HQ17 Airfoil (x,y) Co-ordinates

0 0
0.00235 0.00657
0.00704 0.01408
0.01642 0.02346
0.02581 0.0313
0.03519 0.03754
0.04458 0.04317
0.05397 0.04786
0.06335 0.05256
0.08212 0.061
0.10089 0.06851
0.12905 0.0779
0.1572 0.0862
0.18536 0.0933
0.21351 0.0992
0.24167 0.1043
0.26983 0.10887
0.29798 0.11262
0.32614 0.11544
0.3496 0.1176
0.37306 0.11919
0.39653 0.1205
0.41999 0.1212
0.44345 0.1212
0.46692 0.121
0.49038 0.1203
0.51384 0.1191
0.53731 0.11732
0.56077 0.1149
0.58423 0.112
0.6077 0.10887
0.63116 0.10511
0.65462 0.10042
0.67809 0.09573
0.70155 0.0901
0.72501 0.0845
0.74847 0.0779
0.77194 0.07133
0.7954 0.06382
0.81886 0.05631
0.84233 0.0485
0.86579 0.0413
0.88925 0.0335
0.91272 0.0257
0.93618 0.01877
0.95964 0.0115
0.98311 0.00469
1 0
0.98311 0.001
0.95964 0.0025
0.93618 0.0037
0.91272 0.0042
0.88925 0.00375
0.86579 0.00188
0.84233 -0.0014
0.81886 -0.00469
0.7954 -0.00845
0.77194 -0.0115
0.74847 -0.0148
0.72501 -0.0175
0.70155 -0.0198
0.67809 -0.0218
0.65462 -0.0236
0.63116 -0.025
0.6077 -0.0264
0.58423 -0.0275
0.56077 -0.0285
0.53731 -0.0293
0.51384 -0.03003
0.49038 -0.0306
0.46692 -0.0309
0.44345 -0.03097
0.41999 -0.03097
0.39653 -0.03097
0.37306 -0.0309
0.3496 -0.0309
0.32614 -0.0307
0.29798 -0.0302
0.26983 -0.0297
0.24167 -0.029
0.21351 -0.0282
0.18536 -0.0274
0.1572 -0.0264
0.12905 -0.0252
0.10089 -0.0236
0.08212 -0.0221
0.06335 -0.0202
0.05397 -0.0189
0.04458 -0.0175
0.03519 -0.01595
0.02581 -0.01408
0.01642 -0.0118
0.00704 -0.00845
0.00235 -0.00469
0 0

 

HQ17 Airfoil CAD files

DOWNLOAD FROM HERE

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