Swept shock/boundary-layer interactions - Tutorial and update
作者： G. SETTLES , D. DOLLING
DOI: 10.2514/6.1990-375
关键词:
摘要:
sci-hub.se 参考文章(35)
Gary S. Settles, Hsueh-Ying Teng, Cylindrical and conical flow regimes of three-dimensional shock/boundary-layer interactions AIAA Journal. ,vol. 22, pp. 194- 200 ,(1984) , 10.2514/3.8367
K. H. Token, Heat Transfer Due to Shock Wave Turbulent Boundary Layer Interactions on High Speed Weapon Systems mcdd. ,(1974) , 10.21236/ADA002685
G. S. Settles, C. C. Horstman, T. M. McKenzie, Experimental and computational study of a swept compression corner interaction flowfield AIAA Journal. ,vol. 24, pp. 744- 752 ,(1986) , 10.2514/3.9341
C.C. HORSTMAN, F.K. OWEN, New diagnostic technique for the study of turbulent boundary-layer separation AIAA Journal. ,vol. 12, pp. 1436- 1438 ,(1974) , 10.2514/3.49511
G. N. Kumar, R. I. Vachon, Comparison of three radiative formulations for interactions in three-dimensional boundary layers AIAA Journal. ,vol. 22, pp. 1154- 1161 ,(1984) , 10.2514/3.48554
FRANK LU, GARY SETTLES, Upstream-influence scaling of fin-generated shock wave boundary-layer interactions 28th Aerospace Sciences Meeting, 1990. ,(1990) , 10.2514/6.1990-376
A. Brosh, M. I. Kussoy, C. M. Hung, Experimental and numerical investigation of a shock wave impingementon a cylinder AIAA Journal. ,vol. 23, pp. 840- 846 ,(1985) , 10.2514/3.8996
Oktay Ozcan, Maurice Holt, Supersonic Separated Flow past a Cylindrical Obstacle on a Flat Plate AIAA Journal. ,vol. 22, pp. 611- 617 ,(1984) , 10.2514/3.48492
Doyle D. Knight, C. C. Horstman, Brian Shapey, Seymour Bogdonoff, Structure of supersonic turbulent flow past a sharp fin AIAA Journal. ,vol. 25, pp. 1331- 1337 ,(1987) , 10.2514/3.9787
Gary S. Settles, Frank K. Lu, Conical similarity of shock/boundary-layer interactions generated byswept and unswept fins AIAA Journal. ,vol. 23, pp. 1021- 1027 ,(1985) , 10.2514/3.9033