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Results: 1-25/35
Authors:
ERICSSON LE
BEYERS ME
Citation: Le. Ericsson et Me. Beyers, WIND-TUNNEL AERODYNAMICS IN ROTARY TESTS OF COMBAT AIRCRAFT MODELS, Journal of aircraft, 35(4), 1998, pp. 521-528
Authors:
ERICSSON LE
Citation: Le. Ericsson, HAMMERHEAD WAKE EFFECTS ON ELASTIC VEHICLE DYNAMICS, Journal of spacecraft and rockets, 34(2), 1997, pp. 145-151
Authors:
ERICSSON LE
Citation: Le. Ericsson, ANALYSIS OF THE EFFECT OF SIDESLIP ON DELTA-WING ROLL-TRIM CHARACTERISTICS, Journal of aircraft, 34(5), 1997, pp. 585-591
Authors:
ERICSSON LE
Citation: Le. Ericsson, EFFECT OF ANGLE-OF-ATTACK ON ROLL CHARACTERISTICS OF 65-DEGREE DELTA-WING, Journal of aircraft, 34(4), 1997, pp. 573-575
Authors:
ERICSSON LE
BEYERS ME
Citation: Le. Ericsson et Me. Beyers, CONCEPTUAL FLUID MOTION COUPLING IN THE HERBST SUPERMANEUVER/, Journal of aircraft, 34(3), 1997, pp. 271-277
Authors:
ERICSSON LE
Citation: Le. Ericsson, PARTIAL-SPAN LEADING-EDGE VORTEX CHARACTERISTICS IN HIGH-RATE OSCILLATIONS IN PITCH, Journal of aircraft, 34(3), 1997, pp. 443-445
Authors:
ERICSSON LE
Citation: Le. Ericsson, EFFECT OF DEEP-STALL WING DYNAMICS ON FOREBODY-INDUCED WING ROCK, Journal of aircraft, 34(3), 1997, pp. 448-450
Authors:
ERICSSON LE
Citation: Le. Ericsson, IMPACT OF INITIAL CONDITIONS ON VORTEX BREAKDOWN ON PITCHING DELTA-WINGS, Journal of aircraft, 34(3), 1997, pp. 452-454
Authors:
ERICSSON LE
Citation: Le. Ericsson, PITCH RATE EFFECTS ON DELTA-WING VORTEX BREAKDOWN (VOL 33, PG 639, 1996), Journal of aircraft, 34(2), 1997, pp. 264-264
Authors:
ERICSSON LE
Citation: Le. Ericsson, MOVING WALL EFFECTS CAUSING FLUIDELASTIC INSTABILITY, Journal of aircraft, 34(1), 1997, pp. 23-28
Authors:
ERICSSON LE
Citation: Le. Ericsson, DYNAMIC AIRFOIL FLOW SEPARATION AND REATTACHMENT - REPLY, Journal of aircraft, 33(6), 1996, pp. 1211-1212
Authors:
ERICSSON LE
BEYERS ME
Citation: Le. Ericsson et Me. Beyers, FLAT SPIN OF A CIRCULAR-CYLINDER, Journal of aircraft, 33(4), 1996, pp. 722-729
Authors:
ERICSSON LE
Citation: Le. Ericsson, DIFFICULTIES IN PREDICTING VORTEX BREAKDOWN EFFECTS ON A ROLLING DELTA-WING, Journal of aircraft, 33(3), 1996, pp. 477-484
Authors:
ERICSSON LE
Citation: Le. Ericsson, PITCH RATE EFFECTS ON DELTA-WING VORTEX BREAKDOWN, Journal of aircraft, 33(3), 1996, pp. 639-642
Authors:
ERICSSON LE
MENDENHALL MR
PERKINS SC
Citation: Le. Ericsson et al., REVIEW OF FOREBODY-INDUCED WING ROCK, Journal of aircraft, 33(2), 1996, pp. 253-259
Authors:
ERICSSON LE
Citation: Le. Ericsson, SEPARATED FLOW MECHANISMS IN F-18 WING ROCK, Journal of aircraft, 33(1), 1996, pp. 81-86
Authors:
ERICSSON LE
BEYERS ME
Citation: Le. Ericsson et Me. Beyers, GROUND FACILITY INTERFERENCE EFFECTS ON SLENDER VEHICLE UNSTEADY AERODYNAMICS, Journal of aircraft, 33(1), 1996, pp. 117-124
Authors:
REDING JP
ERICSSON LE
Citation: Jp. Reding et Le. Ericsson, HAMMERHEAD AND NOSE-CYLINDER-FLARE AEROELASTIC STABILITY REVISITED, Journal of spacecraft and rockets, 32(1), 1995, pp. 55-59
Authors:
ERICSSON LE
Citation: Le. Ericsson, DYNAMIC AIRFOIL FLOW SEPARATION AND REATTACHMENT, Journal of aircraft, 32(6), 1995, pp. 1191-1197
Authors:
ERICSSON LE
BEYERS ME
Citation: Le. Ericsson et Me. Beyers, FLAT SPIN OF AXISYMMETRICAL BODIES, Journal of aircraft, 32(6), 1995, pp. 1205-1212
Authors:
ERICSSON LE
Citation: Le. Ericsson, WING ROCK ANALYSIS OF SLENDER DELTA-WINGS, REVIEW AND EXTENSION, Journal of aircraft, 32(6), 1995, pp. 1221-1226
Authors:
ERICSSON LE
Citation: Le. Ericsson, FLOW PHYSICS OF CRITICAL STATES FOR ROLLING DELTA-WINGS, Journal of aircraft, 32(3), 1995, pp. 603-610
Authors:
ERICSSON LE
Citation: Le. Ericsson, COBRA MANEUVER UNSTEADY AERODYNAMIC CONSIDERATIONS, Journal of aircraft, 32(1), 1995, pp. 214-216
Authors:
ERICSSON LE
Citation: Le. Ericsson, MOVING WALL EFFECT IN RELATION TO OTHER DYNAMIC STALL FLOW MECHANISMS, Journal of aircraft, 31(6), 1994, pp. 1303-1309
Authors:
ERICSSON LE
HANFF ES
Citation: Le. Ericsson et Es. Hanff, FURTHER ANALYSIS OF HIGH-RATE ROLLING EXPERIMENTS OF A 65-DEG DELTA-WING, Journal of aircraft, 31(6), 1994, pp. 1350-1357