RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il)
RYAN BQM-34 FIREBEE WING AIRFOIL - Ryan BQM-34 Firebee wing airfoil (NACA 63-014A W/NACA 0014 nose and thinned to .09899 to account for sweep)
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(bqm34-il) RYAN BQM-34 FIREBEE WING AIRFOIL Ryan BQM-34 Firebee wing airfoil (NACA 63-014A W/NACA 0014 nose and thinned to .09899 to account for sweep) Max thickness 9.9% at 32.5% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RYAN BQM-34 FIREBEE WING AIRFOIL
45. 45.
0.0000000 0.0000000
0.0012740 0.0051850
0.0050890 0.0099999
0.0114270 0.0146679
0.0202540 0.0191428
0.0315250 0.0233938
0.0451840 0.0273973
0.0611610 0.0311273
0.0793730 0.0345580
0.0997290 0.0376642
0.1221250 0.0404242
0.1464470 0.0428243
0.1725700 0.0448654
0.2003610 0.0465493
0.2296800 0.0478668
0.2603760 0.0488054
0.2922930 0.0493530
0.3252680 0.0494975
0.3591340 0.0492319
0.3937170 0.0485536
0.4288430 0.0474661
0.4643310 0.0459796
0.5000000 0.0441159
0.5356700 0.0419132
0.5711580 0.0394233
0.6062830 0.0366959
0.6408660 0.0337888
0.6747320 0.0307696
0.7077080 0.0277090
0.7396250 0.0246820
0.7703210 0.0217567
0.7996390 0.0189698
0.8274300 0.0163337
0.8535540 0.0138566
0.8778750 0.0115514
0.9002710 0.0094290
0.9206270 0.0075017
0.9388400 0.0057784
0.9548160 0.0042673
0.9684750 0.0029765
0.9797470 0.0019116
0.9885730 0.0010779
0.9949110 0.0004796
0.9987260 0.0001201
1.0000000 0.0000000
0.0000000 0.0000000
0.0012740 -.0051850
0.0050890 -.0099999
0.0114270 -.0146679
0.0202540 -.0191428
0.0315250 -.0233938
0.0451840 -.0273973
0.0611610 -.0311273
0.0793730 -.0345580
0.0997290 -.0376642
0.1221250 -.0404242
0.1464470 -.0428243
0.1725700 -.0448654
0.2003610 -.0465493
0.2296800 -.0478668
0.2603760 -.0488054
0.2922930 -.0493530
0.3252680 -.0494975
0.3591340 -.0492319
0.3937170 -.0485536
0.4288430 -.0474661
0.4643310 -.0459796
0.5000000 -.0441159
0.5356700 -.0419132
0.5711580 -.0394233
0.6062830 -.0366959
0.6408660 -.0337888
0.6747320 -.0307696
0.7077080 -.0277090
0.7396250 -.0246820
0.7703210 -.0217567
0.7996390 -.0189698
0.8274300 -.0163337
0.8535540 -.0138566
0.8778750 -.0115514
0.9002710 -.0094290
0.9206270 -.0075017
0.9388400 -.0057784
0.9548160 -.0042673
0.9684750 -.0029765
0.9797470 -.0019116
0.9885730 -.0010779
0.9949110 -.0004796
0.9987260 -.0001201
1.0000000 0.0000000
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Polars for RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| bqm34-il | 50,000 | 9 | 27.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 50,000 | 5 | 26.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 100,000 | 9 | 38.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 100,000 | 5 | 34.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 200,000 | 9 | 48.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 200,000 | 5 | 42.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 500,000 | 9 | 56.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 500,000 | 5 | 58.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 1,000,000 | 9 | 70.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 1,000,000 | 5 | 72.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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