Physical model of the swept shock wave/boundary-layer interaction flowfield
- 1 September 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (9) , 2252-2258
- https://doi.org/10.2514/3.11212
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Skin-friction measurements and computational comparison of swept shock/boundary-layer interactionsAIAA Journal, 1991
- On the quasi-conical flowfield structure of the swept shock wave-turbulent boundary layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- A planar Mie scattering technique for visualizing supersonic mixing flowsExperiments in Fluids, 1991
- Three-dimensional shock wave-turbulent boundary layer interactions generated by a sharp fin at Mach 4Published by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Structure of swept shock wave/boundary-layer interactions using conical shadowgraphyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Swept shock/boundary-layer interactions - Tutorial and updatePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Spanwise propagation of upstream influence in conical swept shock/boundary-layer interactionsAIAA Journal, 1987
- Conical similarity of shock/boundary-layer interactions generated byswept and unswept finsAIAA Journal, 1985
- On the size, shape, and orientation of noctilucent cloud particlesTellus B: Chemical and Physical Meteorology, 1983
- Two-wavelength laser transmissometer for measurements of the mean size and concentration of coal ash droplets in combustion flowsApplied Optics, 1980