Investigation of flow variables over a series of rearward facing stepped flat plates at a nominal Mach number of 4.15.
Contributors: Air Force Flight Dynamics Laboratory (U.S.)
Series: Technical documentary report ASD-TDR -- no. 63-131.; Technical documentary report (Air Force Flight Dynamics Laboratory (U.S.)) -- no. 63-131.
Publisher: Wright-Patterson Air Force Base
Published: 1963
Place of publication: [Ohio]
Language: eng
Number of pages: 73
Subjects: Aerodynamics -- Flow.
Notes: "Project no. 1366, task no. 136607."