Water Table Simulation of Subsonic Channel Flow.
Abstract
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1972
- Accession Number
- AD0749134
Entities
People
- Donald P. Mcerlean
- Douglas C. Rabe
- Richard B. Rivir
- William H. Heiser
Organizations
- Air Force Research Laboratory