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Investigation of Hypersonic Inlet Shock-Wave Boundary Layer Interaction: Part II - Continuous Flow Test and Analyses
Author(s): Brown, David L., Hoelmer, Werner, Kutschenreuter, Paul H., Jr.
Corporate Author(s): General Electric Company
Laboratory: Air Force Flight Dynamics Laboratory
Report number: AFFDL TR 65-36
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Design Analysis Summary Of Two Force-Balance Hypersonic Inlet Configurations
Author(s): Kutschenreuter, Paul H., Jr., Balent, Richard L., Richy, George K.
Corporate Author(s): Air Force Flight Dynamics Lab Wright-Patterson Afb Ohio
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-03
Report number: FDL TDR 64-19
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Force Balance Determination of Inlet Performance for Advanced Vehicle Applications to Orbital Velocities Using Internal Drag Measurements
Author(s): Kutschenreuter, Paul H., Jr.
Corporate Author(s): Aeronautical Systems Division
Laboratory: Aeronautical Systems Division
Date of Publication: 1963-09
Report number: ASD TDR 63-701