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Results:
1-9
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Results: 9
Authors:
HEBBAR SK
PLATZER MF
CHANG WH
Citation: Sk. Hebbar et al., CONTROL OF HIGH-INCIDENCE VORTICAL FLOW ON DOUBLE-DELTA WINGS UNDERGOING SIDESLIP, Journal of aircraft, 34(4), 1997, pp. 506-513
Authors:
HEBBAR SK
PLATZER MF
ALKHOZAM AM
Citation: Sk. Hebbar et al., EXPERIMENTAL-STUDY OF VORTEX FLOW-CONTROL ON DOUBLE-DELTA WINGS USINGFILLETS, Journal of aircraft, 33(4), 1996, pp. 743-751
Authors:
HEBBAR SK
PLATZER MF
SMITH EH
SALAZAR ME
Citation: Sk. Hebbar et al., HIGH-ANGLE-OF-ATTACK WIND-TUNNEL INVESTIGATION OF A MULTIMISSION VEHICLE, Journal of spacecraft and rockets, 32(4), 1995, pp. 734-736
Authors:
HEBBAR SK
PLATZER MF
LIU DM
Citation: Sk. Hebbar et al., EFFECT OF CANARD OSCILLATIONS ON AN X-31A-LIKE MODEL IN PITCHING MANEUVER, Journal of aircraft, 32(5), 1995, pp. 1157-1160
Authors:
HEBBAR SK
PLATZER MF
FRINK WD
Citation: Sk. Hebbar et al., EFFECT OF LEADING-EDGE EXTENSION FENCES ON THE VORTEX WAKE OF AN F A-18 MODEL/, Journal of aircraft, 32(3), 1995, pp. 680-682
Authors:
SMITH EH
HEBBAR SK
PLATZER MF
Citation: Eh. Smith et al., AERODYNAMIC CHARACTERISTICS OF A CANARD-CONTROLLED MISSILE AT HIGH ANGLES OF ATTACK, Journal of spacecraft and rockets, 31(5), 1994, pp. 766-772
Authors:
HEBBAR SK
PLATZER MF
KIM CH
Citation: Sk. Hebbar et al., EXPERIMENTAL INVESTIGATION OF VORTEX BREAKDOWN OVER A SIDESLIPPING CANARD-CONFIGURED AIRCRAFT MODEL, Journal of aircraft, 31(4), 1994, pp. 998-1001
Authors:
DIBHAJJ SD
BOULANGER SC
HEBBAR SK
PEEBLES CL
FRANZEN JS
PERLMAN PS
Citation: Sd. Dibhajj et al., DOMAIN-5 INTERACTS WITH DOMAIN-6 AND INFLUENCES THE 2ND TRANSESTERIFICATION REACTION OF GROUP-II INTRON SELF-SPLICING, Nucleic acids research, 21(8), 1993, pp. 1797-1804
Authors:
HEBBAR SK
PLATZER MF
KWON HM
Citation: Sk. Hebbar et al., VORTEX BREAKDOWN STUDIES OF A CANARD-CONFIGURED X-31A-LIKE FIGHTER AIRCRAFT MODEL, Journal of aircraft, 30(3), 1993, pp. 405-408
Risultati:
1-9
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