Search

1 item

application/pdf thumbnail
full text available
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

Refine your search

Refine your search