Skin friction measurements by laser interferometry in swept shock/boundary-layer interactions
- 1 January 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (1), 133-139
- https://doi.org/10.2514/3.10363
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Mach number effects on conical surface features of swept shock boundary-layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Recent skin friction techniques for compressible flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A Laser Interferometer for Measuring Skin Friction in Three-Dimensional FlowsAIAA Journal, 1984
- Flow visualization methods for separated three-dimensional shock wave/turbulent boundary-layer interactionsAIAA Journal, 1983
- A nonintrusive laser interferometer method for measurement of skin frictionExperiments in Fluids, 1983
- Skin Friction Measurements by a Dual-Laser-Beam Interferometer TechniqueAIAA Journal, 1981
- The application of Fizeau interferometry of oil films to the study of surface flow phenomenaOptics and Lasers in Engineering, 1981
- An outline of the techniques available for the measurement of skin friction in turbulent boundary layersProgress in Aerospace Sciences, 1979
- 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
- A modified wall wake velocity profile for turbulent compressible boundary layers.Journal of Aircraft, 1973