Theoretical and experimental studies have shown substantial potential of supersonic combustion with simple engine configuration, i.e. scramjet; description of 50-Mw hypersonic wind tunnel constructed within U S Air Force Flight Dynamics Laboratory (AFFDL) initially designed for research in hypersonic aerodynamic heating; need for research on hydrogen-burning supersonic combustion engine led to augmenting scope of 50-Mw facility, permitting testing of engines under conditions simulating Mach 6 to 12 cruise-flight condition; scramjet structural aspects are outlined.
Building scramjet hypersonic vehicles from ground up
Astronautics Aeronautics
Astronautics and Aeronautics ; 3 , n 10
1965
5 pages
Article (Journal)
English
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