HS1606

HS1 family of prop airfoils

HS1606 Airofil (x,y) Co-ordinates

0 0.00015
0.0005 0.00259
0.001 0.00379
0.002 0.00562
0.003 0.00708
0.005 0.00938
0.0075 0.01164
0.01 0.01352
0.02 0.01926
0.03 0.02371
0.04 0.02756
0.05 0.03105
0.06 0.03429
0.07 0.03731
0.08 0.04012
0.09 0.04273
0.1 0.04515
0.12 0.04946
0.14 0.05318
0.16 0.05638
0.18 0.05915
0.2 0.06153
0.22 0.06354
0.24 0.06522
0.26 0.06659
0.28 0.06772
0.3 0.06865
0.34 0.07005
0.36 0.07056
0.38 0.07092
0.4 0.07112
0.44 0.071
0.46 0.07069
0.48 0.07021
0.5 0.06959
0.54 0.06796
0.56 0.06695
0.58 0.06578
0.6 0.06442
0.64 0.06098
0.66 0.05886
0.68 0.05647
0.7 0.05383
0.74 0.04794
0.76 0.04474
0.78 0.04142
0.8 0.03802
0.82 0.03453
0.84 0.03099
0.86 0.02738
0.88 0.02371
0.9 0.01996
0.91 0.01804
0.92 0.01616
0.93 0.01411
0.94 0.01209
0.95 0.01001
0.96 0.00788
0.97 0.0057
0.98 0.00346
0.99 0.00118
1 -0.00115
1 -0.00589
0.99 -0.00508
0.98 -0.00425
0.97 -0.00346
0.96 -0.00289
0.95 -0.00193
0.94 -0.00119
0.93 -0.00046
0.92 0.00025
0.91 0.00094
0.9 0.00161
0.88 0.00288
0.86 0.00408
0.84 0.00522
0.82 0.0063
0.8 0.00734
0.78 0.00835
0.76 0.0093
0.74 0.01018
0.7 0.01165
0.68 0.01224
0.66 0.01273
0.64 0.01314
0.6 0.01373
0.58 0.01394
0.56 0.01409
0.54 0.0142
0.5 0.01425
0.48 0.01419
0.46 0.01406
0.44 0.01387
0.4 0.01326
0.38 0.01284
0.36 0.01231
0.34 0.01167
0.3 0.00992
0.28 0.00875
0.26 0.00734
0.24 0.00565
0.22 0.00367
0.2 0.00143
0.18 -0.00099
0.16 -0.00347
0.14 -0.00588
0.12 -0.00807
0.1 -0.00988
0.09 -0.0106
0.08 -0.01118
0.07 -0.01161
0.06 -0.01187
0.05 -0.0119
0.04 -0.0116
0.03 -0.01079
0.02 -0.00925
0.01 -0.00656
0.0075 -0.00563
0.005 -0.00455
0.003 -0.00354
0.002 -0.00296
0.001 -0.0022
0.0005 -0.00162
0 0.00015

HS1606 Airfoil CAD files

DOWNLOAD FROM HERE

Leave a Reply