Water Table Simulation of Subsonic Channel Flow.
Technical rept. Jul-Nov 71,
AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OHIO
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The report presents the results obtained from a test program designed to simulate the flow of a compressible gas through a channel of varying cross section and wall contour through the use of the water analogy. All flows which were simulated had nominal values of free-stream Mach numbers between 0.1 and 0.6. Author
- Lasers and Masers
- Fluid Mechanics