FWind Posted November 30, 2019 Posted November 30, 2019 (edited) There two document and a video about the max AOA of the F-14: 1. AIAA-1983-1051 Variable sweep wing design The max AOA in this file is 77 degrees. https://youtu.be/Ci_Y_PLUnuI?t=375 https://youtu.be/Ci_Y_PLUnuI?t=119 2.AIAA-81-2505 Flight test experience with high-alpha control system techniques on the F-14 airplane AOA of 74 degrees in clean configuration, and AOA of 62 degrees external stores configuartion. could the maximum angle of attack exceed 70 degrees after the completion of the FM? Edited December 8, 2019 by FWind
captain_dalan Posted December 2, 2019 Posted December 2, 2019 There two document and a video about the max AOA of the F-14: 1. AIAA-1983-1051 Variable sweep wing design The max AOA in this file is 77 degrees. [ATTACH]222038[/ATTACH] https://youtu.be/Ci_Y_PLUnuI?t=375 2.AIAA-81-2505 Flight test experience with high-alpha control system techniques on the F-14 airplane AOA of 74 degrees in clean configuration, and AOA of 62 degrees external stores configuartion. [ATTACH]222034[/ATTACH] [ATTACH]222035[/ATTACH] [ATTACH]222036[/ATTACH] The Max AOA of F-14 is 50 degrees in DCS. could the maximum angle of attack exceed 70 degrees after the completion of the FM? I think that to go above 50 you need to enter the transitional region (when the wings are stalled but the body still produces enough lift) and this is in general not a sustainable state. I haven't really tried to get her there yet, but try testing her with some gravity assisted maneuvers. :pilotfly: Modules: FC3, Mirage 2000C, Harrier AV-8B NA, F-5, AJS-37 Viggen, F-14B, F-14A, Combined Arms, F/A-18C, F-16C, MiG-19P, F-86, MiG-15, FW-190A, Spitfire Mk IX, UH-1 Huey, Su-25, P-51PD, Caucasus map, Nevada map, Persian Gulf map, Marianas map, Syria Map, Super Carrier, Sinai map, Mosquito, P-51, AH-64 Apache
FWind Posted December 2, 2019 Author Posted December 2, 2019 I think that to go above 50 you need to enter the transitional region (when the wings are stalled but the body still produces enough lift) and this is in general not a sustainable state. I haven't really tried to get her there yet, but try testing her with some gravity assisted maneuvers. :pilotfly: :pilotfly::(
jcdata Posted December 3, 2019 Posted December 3, 2019 Those docs bring back memories working on fd for the tomcat. Above 35k or so typically, the f110 tomcat during stall testing exhibited 60 deg... Is it usable? No Sent from my SM-N950U using Tapatalk
FWind Posted December 5, 2019 Author Posted December 5, 2019 Those docs bring back memories working on fd for the tomcat. Above 35k or so typically, the f110 tomcat during stall testing exhibited 60 deg... Is it usable? No Sent from my SM-N950U using Tapatalk But it cool.:smartass:
jcdata Posted December 5, 2019 Posted December 5, 2019 I can achieve 58.5 deg AoA @ 35,800 ft: Boom! Sent from my SM-N950U using Tapatalk
FWind Posted December 5, 2019 Author Posted December 5, 2019 :thumbup: I can achieve 58.5 deg AoA @ 35,800 ft:
FWind Posted December 8, 2019 Author Posted December 8, 2019 (edited) I can achieve 58.5 deg AoA @ 35,800 ft: Around 35000ft and speed at Mach0.4-0.7 in level flight, full aft stick, the max AoA is 52.3 deg. Tacview-20191208-095230-DCS-test.zip Edited December 8, 2019 by FWind
FWind Posted December 8, 2019 Author Posted December 8, 2019 (edited) alt 35000ft around, levle flight, cross control+full aft stick, the max AoA is 66.8 deg. Tacview-20191208-110945-DCS-test.zip test cross control+full aft stick.trk The screen not the max AoA: Edited December 8, 2019 by FWind
FWind Posted December 21, 2019 Author Posted December 21, 2019 Alt 25000ft, Mach 0.55, Cross control + full aft stick, the Max AOA is 73.8 deg. Tacview-20191215-125714-DCS.zip
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