F-14A low altitude high angle of attack simulation and flight test program

1986 ◽  
Author(s):  
R. GOODMAN ◽  
P. CONIGLIARO
Keyword(s):  
Angle Of Attack ◽  
Flight Test ◽  
High Angle ◽  
Test Program ◽  
High Angle Of Attack ◽  
Low Altitude

KEEP EAGLE F-15E High Angle-of-Attack Flight Test Program

1997 ◽  
Vol 34 (3) ◽  
pp. 265-270
Author(s):  
David M. Sitz ◽  
David C. Nelson ◽  
Mark R. Carpenter
Keyword(s):  
Angle Of Attack ◽  
Flight Test ◽  
High Angle ◽  
Test Program ◽  
High Angle Of Attack

The KEEP EAGLE F-15E High Angle-of-Attack Flight Test Program

1996 ◽  
Author(s):  
Mark R. Carpenter ◽  
David M. Sitz ◽  
David C. Nelson
Keyword(s):  
Angle Of Attack ◽  
Flight Test ◽  
High Angle ◽  
Test Program ◽  
High Angle Of Attack

scholarly journals Research on high attack angle stall and spin characteristics with flight test of a general electric aircraft

2021 ◽  
Vol 39 (3) ◽  
pp. 650-659
Author(s):  
Yadong Li ◽  
Junyao Zhang ◽  
Fengtian Yang ◽  
Yongliang Chen
Keyword(s):  
Numerical Simulation ◽  
Aspect Ratio ◽  
Aerodynamic Force ◽  
Angle Of Attack ◽  
Wind Tunnel Test ◽  
Flight Test ◽  
High Angle ◽  
High Angle Of Attack ◽  
Linear Change ◽  
Electric Aircraft

When the aircraft is flying at high angle of attack, the local separation of the air flow on the surface of the aircraft, the linear change of aerodynamic force is destroyed, and the maneuverability and stability are reduced to varying degrees, resulting in the aircraft stalling or entering the spin. The stall characteristics and spin characteristics directly affect the safety of the aircraft. In order to analyze the stall and spin characteristics, a full-scale 6-DOF nonlinear high angle of attack dynamic model is established for a two-seater electric high aspect ratio aircraft based on the wind tunnel test data. The stall characteristics of an electric aircraft at high angle of attack are obtained by numerical simulation and analysis. According to the stall characteristics of simulation calculation, flight test is carried out to verify the reliability of numerical simulation, which provides reference for the later analysis of stall/spin test of large aspect ratio series electric aircraft at nonlinear high angle of attack.

Sign in / Sign up

Export Citation Format

Share Document