共 50 条
- [31] SUBSONIC VORTEX-FLOW DESIGN STUDY FOR SLENDER WINGS JOURNAL OF AIRCRAFT, 1978, 15 (09): : 611 - 617
- [33] New model for high angle-of-attack motion of an aircraft Xibei Gongye Daxue Xuebao, 4 (553-557):
- [34] HIGH ANGLE-OF-ATTACK FLUSH AIRDATA SENSING SYSTEM JOURNAL OF AIRCRAFT, 1992, 29 (05): : 915 - 919
- [35] Aerodynamic Test Study on Slender Air Vehicle at Extra-Wide Angle-of-Attack 2023 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL II, APISAT 2023, 2024, 1051 : 1945 - 1953
- [37] Numerical studies of asymmetric vortex flows around a slender body at high angle of attack MODERN PHYSICS LETTERS B, 2005, 19 (28-29): : 1463 - 1466
- [40] CALCULATION OF HIGH ANGLE-OF-ATTACK AERODYNAMICS OF FIGHTER CONFIGURATIONS AIAA 7TH APPLIED AERODYNAMICS CONFERENCE: A COLLECTION OF TECHNICAL PAPERS, 1989, : 205 - 217