共 50 条
- [21] SUPERSONIC BOUNDARY-LAYER STABILITY ANALYSIS ON AN AIRCRAFT WING JOURNAL OF AIRCRAFT, 1991, 28 (11): : 721 - 727
- [23] Three-dimensional boundary-layer transition on a swept wing at Mach 3.5 Cattafesta, L.M.III, 1600, (33):
- [25] STATUS OF LINEAR BOUNDARY-LAYER STABILITY THEORY AND THE en METHOD, WITH EMPHASIS ON SWEPT-WING APPLICATIONS. NASA Technical Paper, 1980, (1645):
- [26] Boundary-layer transition on a swept cylinder Reports of the Laboratory for Air-Flow Measurements, the Institute of High Speed Mechanics, Tohoku University, 1988, 4
- [27] Interactive Three-Dimensional boundary-layer method for transonic flow over swept wings Woodson, Shawn H., 1600, (29):
- [29] Nonequilibrium-dissociated stagnation boundary-layer flow on an arbitrarily catalytic swept wing Inger, G.R., 1836, American Inst. Aeronautics and Astronautics Inc., United States (33):