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Results: 26-35/35
Authors:
ERICSSON LE
Citation: Le. Ericsson, PROBLEM OF DYNAMIC STALL SIMULATION REVISITED, Journal of aircraft, 31(4), 1994, pp. 782-786
Authors:
ERICSSON LE
Citation: Le. Ericsson, EFFECT OF FUSELAGE ON DELTA-WING VORTEX BREAKDOWN - COMMENT, Journal of aircraft, 31(4), 1994, pp. 1006-1007
Authors:
ERICSSON LE
HANFF ES
Citation: Le. Ericsson et Es. Hanff, UNIQUE HIGH-ALPHA ROLL DYNAMICS OF A SHARP-EDGED 65-DEG DELTA-WING, Journal of aircraft, 31(3), 1994, pp. 520-525
Authors:
ERICSSON LE
Citation: Le. Ericsson, CONTROL OF VORTICES ON A DELTA-WING BY LEADING-EDGE INJECTION, AIAA journal, 32(10), 1994, pp. 2134-2135
Authors:
ERICSSON LE
Citation: Le. Ericsson, UNSTEADY-FLOW SEPARATION ON SLENDER BODIES AT HIGH ANGLES OF ATTACK, Journal of spacecraft and rockets, 30(6), 1993, pp. 689-695
Authors:
ERICSSON LE
KING HHC
Citation: Le. Ericsson et Hhc. King, EXTENSION OF UNSTEADY EMBEDDED NEWTONIAN THEORY, Journal of spacecraft and rockets, 30(3), 1993, pp. 316-322
Authors:
BEYERS ME
ERICSSON LE
Citation: Me. Beyers et Le. Ericsson, GROUND FACILITY INTERFERENCE ON AIRCRAFT CONFIGURATIONS WITH SEPARATED FLOW, Journal of aircraft, 30(5), 1993, pp. 682-688
Authors:
ERICSSON LE
KING HHC
Citation: Le. Ericsson et Hhc. King, EFFECT OF LEADING-EDGE GEOMETRY ON DELTA-WING UNSTEADY AERODYNAMICS, Journal of aircraft, 30(5), 1993, pp. 793-795
Authors:
ERICSSON LE
Citation: Le. Ericsson, SLENDER WING ROCK REVISITED, Journal of aircraft, 30(3), 1993, pp. 352-356
Authors:
ERICSSON LE
Citation: Le. Ericsson, THOUGHTS ON CONICAL FLOW ASYMMETRY, AIAA journal, 31(9), 1993, pp. 1563-1568