Skin-friction measurements in three-dimensional, supersonic shock-wave/boundary-layer interaction
- 1 May 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (5), 805-811
- https://doi.org/10.2514/3.12503
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Low Aspect Ratio Wing Code Validation ExperimentAIAA Journal, 1993
- Boundary-Layer Transition and Global Skin Friction Measurement with an Oil-Fringe Imaging TechniqueSAE International Journal of Advances and Current Practices in Mobility, 1993
- Two-directional skin friction measurement utilizing a compact internally mounted thin-liquid-film skin friction meterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Calculation of a three-dimensional shock wave-turbulent boundary-layer interactionAIAA Journal, 1990
- Skin friction measurements by laser interferometry in swept shock/boundary-layer interactionsAIAA Journal, 1990
- Two-component LDV investigation of three-dimensional shock/turbulentboundary-layer interactionsAIAA Journal, 1988
- Holographic interferometry study of an axisymmetric shock-wave/boundary-layer strong interaction flowAIAA Journal, 1987
- Topological classification of flow separation on three-dimensional bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A study of the motion of oil films on surfaces in air flow, with application to the measurement of skin frictionJournal of Physics E: Scientific Instruments, 1976