Short-duration test facility obtains extremely high Reynolds number flows in subsonic, transonic, and supersonic speed ranges, and aids in solving Reynolds number-dependent aerodynamic and thermodynamic problems in design and testing of large, high speed vehicles. The modified blowdown wind tunnel avoids data confusion and aerodynamic noise.
Short-duration, transonic flow, variable-porosity test section
01.09.1970
Sonstige
Keine Angabe
Englisch
Variable porosity walls for transonic wind tunnels
NTRS | 1965
|Transonic Flow at a Slotted Test Section Wall
NTIS | 1975
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