Pitch rate effects on delta wing vortex breakdown

[1] [Anonymous], 3282 RM AER RES COUN

[2] HYSTERESIS OF VORTEX DEVELOPMENT AND BREAKDOWN ON AN OSCILLATING DELTA-WING [J]. AIAA JOURNAL, 1987, 25 (11) : 1512 - 1513

[3] ATTA R, 1987, AIAA J, V25, P1513

[4] BEYERS ME, 1994, COMMUNICATION JUL

[5] ELLE BJ, 1958, 3176 RM AER RES COUN

[6] APPROXIMATE NONLINEAR SLENDER WING AERODYNAMICS [J]. JOURNAL OF AIRCRAFT, 1977, 14 (12): : 1197 - 1204

[7] FLOW PHYSICS OF CRITICAL STATES FOR ROLLING DELTA-WINGS [J]. JOURNAL OF AIRCRAFT, 1995, 32 (03): : 603 - 610

[8] Difficulties in predicting vortex breakdown effects on a rolling delta wing [J]. JOURNAL OF AIRCRAFT, 1996, 33 (03): : 477 - 484

[9] EFFECT OF LEADING-EDGE GEOMETRY ON DELTA-WING UNSTEADY AERODYNAMICS [J]. JOURNAL OF AIRCRAFT, 1993, 30 (05): : 793 - 795

[10] ERICSSON LE, 1987, PROGR AEROSPACE SCI, V24, P249, DOI DOI 10.1016/0376-0421(87)90001-7PAESD60376-0421

[1] [Anonymous], 3282 RM AER RES COUN

[2] HYSTERESIS OF VORTEX DEVELOPMENT AND BREAKDOWN ON AN OSCILLATING DELTA-WING [J]. AIAA JOURNAL, 1987, 25 (11) : 1512 - 1513

[3] ATTA R, 1987, AIAA J, V25, P1513

[4] BEYERS ME, 1994, COMMUNICATION JUL

[5] ELLE BJ, 1958, 3176 RM AER RES COUN

[6] APPROXIMATE NONLINEAR SLENDER WING AERODYNAMICS [J]. JOURNAL OF AIRCRAFT, 1977, 14 (12): : 1197 - 1204

[7] FLOW PHYSICS OF CRITICAL STATES FOR ROLLING DELTA-WINGS [J]. JOURNAL OF AIRCRAFT, 1995, 32 (03): : 603 - 610

[8] Difficulties in predicting vortex breakdown effects on a rolling delta wing [J]. JOURNAL OF AIRCRAFT, 1996, 33 (03): : 477 - 484

[9] EFFECT OF LEADING-EDGE GEOMETRY ON DELTA-WING UNSTEADY AERODYNAMICS [J]. JOURNAL OF AIRCRAFT, 1993, 30 (05): : 793 - 795

[10] ERICSSON LE, 1987, PROGR AEROSPACE SCI, V24, P249, DOI DOI 10.1016/0376-0421(87)90001-7PAESD60376-0421