Calibration Experience in the Langley Hotshot Tunnel for Mach Numbers from 12 to 26
1966
48 pages
Report
Keine Angabe
Englisch
Laboratory & Test Facility Design & Operation , Arc chamber , Flow characteristics , Rocket nozzle , Arc , Axial , Boundary , Chamber , Characteristics , Coaxial , Diameter , Electrode , Flow , Hypervelocity , Layer , Nozzle , Rocket , Station , Thickness , Throat