McDaniel et al., 2002 - Google Patents
Experimental and computational comparison of an underexpanded jet flowfieldMcDaniel et al., 2002
- Document ID
- 5783604409496551946
- Author
- McDaniel J
- Glass C
- Staack D
- Miller C
- Publication year
- Publication venue
- 40th AIAA Aerospace Sciences Meeting & Exhibit
External Links
Snippet
A hypersonic free jet wind tunnel has been designed and assembled at the University of Virginia to experimentally study rarefied flow phenomena. The purpose of this study is to provide a comparison of experimental and numerical results with theoretical/empirical …
- 238000005259 measurement 0 abstract description 22
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
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