Spanwise propagation of upstream influence in conical swept shock/boundary-layer interactions
- 1 February 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (2) , 287-293
- https://doi.org/10.2514/3.9620
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Similarity of quasiconical shock wave/turbulent boundary-layer interactionsAIAA Journal, 1986
- Conical similarity of shock/boundary-layer interactions generated byswept and unswept finsAIAA Journal, 1985
- Experimental studies of quasi-two-dimensional and three-dimensional viscous interaction regions induced by skewed-shock and swept-shock boundary layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Cylindrical and conical flow regimes of three-dimensional shock/boundary-layer interactionsAIAA Journal, 1984
- Upstream influence in sharp fin-induced shock wave turbulent boundary-layer interactionAIAA Journal, 1983
- An experimental study of the interaction between a glancing shock wave and a turbulent boundary layerJournal of Fluid Mechanics, 1982