共 50 条
- [1] TURBULENT BOUNDARY-LAYER ON A YAWED WING [J]. ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1973, 21 (05): : 163 - 166
- [2] LAMINAR BOUNDARY-LAYER ON A YAWED INFINITE CYLINDER [J]. APPLIED SCIENTIFIC RESEARCH, 1975, 30 (06): : 469 - 476
- [3] THE COMPRESSIBLE LAMINAR BOUNDARY LAYER ON A YAWED INFINITE WING [J]. AERONAUTICAL QUARTERLY, 1954, 5 (02): : 85 - 100
- [4] BOUNDARY-LAYER MEASUREMENTS IN HYPERSONIC FLOW [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (01): : 35 - 42
- [5] ON THE BOUNDARY-LAYER EQUATIONS IN HYPERSONIC FLOW [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (07): : 500 - 501
- [6] 3-DIMENSIONAL TURBULENT BOUNDARY LAYER ON AN INFINITE YAWED WING [J]. AERONAUTICAL QUARTERLY, 1971, 22 (NOV): : 346 - &
- [8] SHOCK WAVE-TURBULENT BOUNDARY-LAYER INTERACTION IN HYPERSONIC FLOW [J]. ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B7 - B7
- [9] EXPERIMENTS ON SHOCK-WAVE BOUNDARY-LAYER INTERACTION IN HYPERSONIC FLOW [J]. RECHERCHE AEROSPATIALE, 1993, (01): : 61 - 74
- [10] Interaction between compliant structures and boundary-layer transition in hypersonic flow [J]. 1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (55):