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Results: 1-13 |
Results: 13
NAVIER-STOKES PREDICTIONS OF PITCH DAMPING FOR AXISYMMETRICAL PROJECTILES
Authors: WEINACHT P STUREK WB SCHIFF LB
Citation: P. Weinacht et al., NAVIER-STOKES PREDICTIONS OF PITCH DAMPING FOR AXISYMMETRICAL PROJECTILES, Journal of spacecraft and rockets, 34(6), 1997, pp. 753-761
COMPUTATION OF F A-18 TAIL BUFFET
Authors: GEE K MURMAN SM SCHIFF LB
Citation: K. Gee et al., COMPUTATION OF F A-18 TAIL BUFFET, Journal of aircraft, 33(6), 1996, pp. 1181-1189
NUMERICAL-SIMULATION OF FORCED AND FREE-TO-ROLL DELTA-WING MOTIONS
Authors: CHADERJIAN NM SCHIFF LB
Citation: Nm. Chaderjian et Lb. Schiff, NUMERICAL-SIMULATION OF FORCED AND FREE-TO-ROLL DELTA-WING MOTIONS, Journal of aircraft, 33(1), 1996, pp. 93-99
ANALYSIS OF TANGENTIAL SLOT BLOWING ON F A-18 ISOLATED FOREBODY/
Authors: GEE K RIZK YM SCHIFF LB
Citation: K. Gee et al., ANALYSIS OF TANGENTIAL SLOT BLOWING ON F A-18 ISOLATED FOREBODY/, Journal of aircraft, 32(5), 1995, pp. 1040-1046
COMPUTATIONAL INVESTIGATION OF TANGENTIAL SLOT BLOWING ON A GENERIC CHINED FOREBODY
Authors: AGOSTAGREENMAN RM GEE K CUMMINGS RM SCHIFF LB
Citation: Rm. Agostagreenman et al., COMPUTATIONAL INVESTIGATION OF TANGENTIAL SLOT BLOWING ON A GENERIC CHINED FOREBODY, Journal of aircraft, 32(4), 1995, pp. 811-817
EXPERIMENTAL INVESTIGATION OF TANGENTIAL SLOT BLOWING ON A GENERIC CHINED FOREBODY
Authors: CUMMINGS RM SCHIFF LB DUINO JD
Citation: Rm. Cummings et al., EXPERIMENTAL INVESTIGATION OF TANGENTIAL SLOT BLOWING ON A GENERIC CHINED FOREBODY, Journal of aircraft, 32(4), 1995, pp. 818-824
NUMERICAL INVESTIGATION OF HIGH-INCIDENCE FLOW OVER A DOUBLE-DELTA WING
Authors: EKATERINARIS JA COUTLEY RL SCHIFF LB PLATZER MF
Citation: Ja. Ekaterinaris et al., NUMERICAL INVESTIGATION OF HIGH-INCIDENCE FLOW OVER A DOUBLE-DELTA WING, Journal of aircraft, 32(3), 1995, pp. 457-463
DIRECTIONAL CONTROL AT HIGH ANGLES OF ATTACK USING BLOWING THROUGH A CHINED FOREBODY
Authors: ARENA AS NELSON RC SCHIFF LB
Citation: As. Arena et al., DIRECTIONAL CONTROL AT HIGH ANGLES OF ATTACK USING BLOWING THROUGH A CHINED FOREBODY, Journal of aircraft, 32(3), 1995, pp. 596-602
NAVIER-STOKES SOLUTION FOR AN OSCILLATING DOUBLE-DELTA WING
Authors: EKATERINARIS JA SCHIFF LB
Citation: Ja. Ekaterinaris et Lb. Schiff, NAVIER-STOKES SOLUTION FOR AN OSCILLATING DOUBLE-DELTA WING, Journal of aircraft, 32(2), 1995, pp. 228-234
NUMERICAL-SIMULATION OF INCIDENCE AND SWEEP EFFECTS ON DELTA-WING VORTEX BREAKDOWN
Authors: EKATERINARIS JA SCHIFF LB
Citation: Ja. Ekaterinaris et Lb. Schiff, NUMERICAL-SIMULATION OF INCIDENCE AND SWEEP EFFECTS ON DELTA-WING VORTEX BREAKDOWN, Journal of aircraft, 31(5), 1994, pp. 1043-1049
FOREBODY TANGENTIAL SLOT BLOWING ON AN AIRCRAFT GEOMETRY
Authors: GEE K RIZK YM SCHIFF LB
Citation: K. Gee et al., FOREBODY TANGENTIAL SLOT BLOWING ON AN AIRCRAFT GEOMETRY, Journal of aircraft, 31(4), 1994, pp. 922-928
NUMERICAL PREDICTION OF VORTICAL FLOW OVER SLENDER DELTA-WINGS
Authors: EKATERINARIS JA SCHIFF LB
Citation: Ja. Ekaterinaris et Lb. Schiff, NUMERICAL PREDICTION OF VORTICAL FLOW OVER SLENDER DELTA-WINGS, Journal of aircraft, 30(6), 1993, pp. 935-942
COMPUTATIONAL INVESTIGATION OF A PNEUMATIC FOREBODY FLOW-CONTROL CONCEPT
Authors: GEE K TAVELLA D SCHIFF LB
Citation: K. Gee et al., COMPUTATIONAL INVESTIGATION OF A PNEUMATIC FOREBODY FLOW-CONTROL CONCEPT, Journal of aircraft, 30(3), 1993, pp. 326-333
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