共 50 条
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- [23] INVESTIGATION OF THE INFLUENCE OF THE BASE ON SUPERSONIC-FLOW AROUND A CONE WITH POWER-LAW INJECTION SOVIET APPLIED MECHANICS, 1979, 15 (08): : 752 - 755
- [24] SUPERSONIC-FLOW PAST A SLENDER DELTA WING - EXPERIMENTAL INVESTIGATION COVERING INCIDENCE RANGE -5DEGREES LESS-THAN-OR-EQUAL-TO ALPHA LESS-THAN-OR-EQUAL-TO 50DEGREES AERONAUTICAL QUARTERLY, 1976, 27 (MAY): : 143 - 153
- [25] TRANSONIC SUPERSONIC-FLOW PAST BLUNT ROTATING BODIES ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1976, 56 (03): : T178 - T181
- [26] THE NUMERICAL INVESTIGATION OF SUPERSONIC-FLOW ALONG THE CIRCULAR CONE WITH PLANE WINGS BY NONVISCOUS GAS-FLOW IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1989, (01): : 53 - 55
- [27] SUPERSONIC-FLOW PAST CIRULAR CONES AT HIGH ANGLES OF YAW, DOWNSTREAM OF SEPARATION LECTURE NOTES IN PHYSICS, 1985, 218 : 277 - 280
- [28] THE OPTIMIZATION OF THE RELAXATION DRAG OF SLENDER PROFILES IN STEADY, PLANE SUPERSONIC-FLOW INGENIEUR ARCHIV, 1981, 50 (04): : 225 - 235
- [29] MITIGATION OF PRESSURE OSCILLATIONS INDUCED BY SUPERSONIC-FLOW OVER SLENDER CAVITIES JOURNAL OF AIRCRAFT, 1992, 29 (06): : 999 - 1004