Pressure Recovery in Rectangular Constant Area Supersonic Diffusers
- 1 February 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (2) , 168-172
- https://doi.org/10.2514/3.61352
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Wall Shear and Boundary-Layer Measurements in Shock Seperated FlowAIAA Journal, 1974
- Structure of Shock Waves in Cylindrical DuctsAIAA Journal, 1973
- Design of a Multipurpose Wind TunnelReview of Scientific Instruments, 1969
- Investigation of the diffusion characteristics of supersonic streamscomposed mainly of boundary layers.Journal of Aircraft, 1965
- Supersonic Diffusers for Wind TunnelsJournal of Applied Mechanics, 1949