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- [2] SIDE-FORCE CONTROL ON A DIAMOND FOREBODY AT HIGH ANGLES OF ATTACKJOURNAL OF AIRCRAFT, 1994, 31 (04): : 915 - 921RAO, DMSHARMA, G
- [3] REDUCTION OF THE SIDE FORCE ON POINTED FOREBODIES THROUGH ADD-ON TIP DEVICESAIAA JOURNAL, 1992, 30 (10) : 2462 - 2468MODI, VJCHENG, CWMAK, AYOKOMIZO, T
- [4] Simulation of flow about rotating forebodies at high angles of attack Saephan, S. (ssaephan@ucdavis.edu), 1600, American Institute of Aeronautics and Astronautics Inc. (41):
- [5] ALLEVIATION OF SIDE FORCE ON TANGENT-OGIVE FOREBODIES USING PASSIVE POROSITYJOURNAL OF AIRCRAFT, 1994, 31 (02): : 354 - 361BAUER, SXSHEMSCH, MJ
- [6] Simulation of flow about rotating forebodies at high angles of attackJOURNAL OF AIRCRAFT, 2004, 41 (06): : 1298 - 1305Saephan, Svan Dam, CPFremaux, CMDalBello, T
- [7] Alleviation of side force on tangent-ogive forebodies using passive porosityJournal of Aircraft, 1994, 31 (02): : 354 - 361Bauer, Steven X.S.Hemsch, Michael J.
- [8] ALLEVIATION OF THE SIDE FORCE AND THE YAWING MOMENT ACTING ON A SLENDER CONE-CYLINDER BODY AT HIGH ANGLES OF ATTACK, USING SMALL JET INJECTION AT SUBSONIC AND TRANSONIC SPEEDS.TAE Report (Technion Israel Institute of Technology, Department of Aeronautical Engineering), 1979, (380):Almosnino, D.Rom, J.
- [9] AERODYNAMICS OF SLENDER BODIES AT HIGH ANGLES OF ATTACKJOURNAL OF SPACECRAFT AND ROCKETS, 1979, 16 (01) : 10 - 14PRZIREMBEL, CEGSHEREDA, DE
- [10] VORTICES ON SLENDER BODIES AT HIGH ANGLES OF ATTACKAERONAUTIQUE ASTRONAUTIQUE, 1979, (79): : 3 - 22WERLE, H