Predicted high-α aerodynamic characteristics of maneuvering aircraft

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 468-476

  Mendenhall, M R ^a   Perkins, S C ^a  

^a Nielsen Engineering & Research Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; ANGLE OF ATTACK; DEGREES OF FREEDOM (MECHANICS); FREE FLIGHT; MANEUVERABILITY; VEHICLES; WIND TUNNELS;

AERODYNAMIC CHARACTERISTICS; ANALYSIS CAPABILITIES; FLIGHT-TEST VEHICLES; GENERIC CONFIGURATION; HIGH ANGLES OF ATTACK; MANEUVERING AIRCRAFTS; PHYSICS-BASED METHODS; PREDICTION CAPABILITY;

AERODYNAMICS;

EID: 84964222900     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Lang, J. and Francis, M. S.: Unsteady Aerodynamics and Dynamic Aircraft Maneuverability. AGARD-CP-386, May 1985.
2. Mendenhall, M. R, Perkins, S. C, Jr., and Ericsson, L. E.: Prediction of Forebody Vortex-Induced Wing Rock on Wing-Body Configurations. AIAA 93-3451, Aug. 1993.
3. Mendenhall, M. R. and Perkins, S. C, Jr..: ComputationalMethodology for Maneuvering Aircraft atHigh Angles of Attack. NEAR TR 508, Mar. 1996.
4. Mendenhall, M. R. and Perkins, S. C, Jr.: An Unsteady Vortex Wake Model for Maneuvering Vehicles. AGARD Symposium on The Characteristics & Modification of Ves from Lifting Vehicles in Fluids. Trondheim, Norway. May 1996.
5. Mendenhall, M. R. and Perkins, S. C, Jr.: Prediction of Vortex-Induced Fluid Mechanics of Maneuvering Submarines. AIAA 93-0638, Jan. 1993.
6. Mendenhall, M. R. and Perkins, S. C, Jr.: Analysis of Dynamic Maneuver Performance of Fighter Aircraft at High Angles of Attack. AFWAL-TR-88-3048, July 1988.
7. Mendenhall, M. R, Perkins, S. C, Jr., and Lesieutre, D. J.: Prediction of the Nonlinear Aerodynamic Characteristics of Maneuvering Missiles. Journal of Spacecraft and Rockets. Vol. 24. Sept-Oct. 1987. pp. 394-402.
8. Mendenhall, M. R., Radons S. C, Jr., and Lesieutre, D. J.: Vortex Cloud Model for Body Vortices and Tracking. Tactical Missile Aerodynamics: Prediction Methodology. Vol. 142 of Progress in Astronautics and Aeronautics, ed by M. R. Mendenhall, AIAA, 1992, pp. 225-285.
9. Carr, LW. and Chandrasekhara, M. S.: An Assessment of the Impact of Compressibility on Dynamic Stall. AIAA 95-0779, Jan. 1995.
10. Niven, A J. and Galbraith, R. A. McD.: Experiments on the Establishment of Fully Attached Airfoil Flow from the Fully Stalled Condition During Ramp-Down Motions. ICAS Paper 90-3.4.3, Sept. 1990.
11. Brandon, J. M. and Nguyen, L. T.: Experimental Study of Effects of Forebody Geometry on High Angle of Attack Static and Dynamic Stability. Journal of Aircraft. Vol. 25, No. 7, July 1988,pp. 591-597.
12. Williams, D.L. 2nd, Nelson, R.C., and Fisher, D.F.: An Investigation of X-31 Roll Characteristics at High Angle-of-Attack Through Subscale Model Testing. AIAA 94-0806, Jan. 1994