1422 - Dec 1947, Wing Number Threeġ8 : Random Wing With 4412 Airfoil Sections, Aspect Ratio = 6Ģ0 : Flat Plate Wing, Aspect Ratio = 2.352Ģ2 : Supersonic Air-to-Air Missile At Mach FourĢ3 : Supersonic Sharp Delta Wing At Mach Six (Airloads older version results)Ģ4 : Supersonic North American XB-70 At Mach 2.4Ģ5 : Supersonic North American XB-70 At Mach 4Ģ6 : Supersonic Arrow wing at mach four, notch ratio = 0.1264Ģ7 : Supersonic Arrow wing at mach three, notch ratio = zeroĢ8 : Supersonic High Aspect Ratio Swept Cambered Wing At Mach 3ģ0 : AIM-7 Short Range Air-to-Air Missile at Mach 4. 1422 - Dec 1947, Wing Number Twoġ7 : NACA TN No. 1422 - Dec 1947, Wing Number Oneġ6 : NACA TN No. 1269 - April 1947, Wing Number Threeġ5 : NACA TN No. 1269 - April 1947, Wing Number Twoġ4 : NACA TN No. 1269 - April 1947, Wing Number Oneġ3 : NACA TN No. 537 - May 1935, Wing Number Nineġ2 : NACA TN No. 537 - May 1935, Wing Number Sevenġ1 : NACA TR No. 537 - May 1935, Wing Number Threeġ0 : NACA TR No. the different airfoils in Table 2, based on the mentioned criteria, S5010 airfoil is chosen as a suitable airfoil for the MAV with C L /C D being equal to 9.89. 537 - May 1935, 23012 Five Series Airfoilħ : NACA TR No. 824 - March 1945, 2412 Four Series AirfoilĦ : NACA TR No. 824 - March 1945, 0015 Symmetric Airfoilĥ : NACA TR No. Test Cases : ( Some Tests With Airloads Older Versions )Ĥ : NACA TR No.
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