Collection
Serial/Series Title
1 Matching Results
Results open in a new window/tab.
Results:
1 - 1 of
1
Investigation of a Two-Step Nozzle in an 11-Inch Hypersonic Tunnel
Report discussing flow surveys made of several nozzles using two 2-dimensional steps at Mach number 6.98. Results regarding wall-pressure surveys, disturbance patterns in expansion, total-pressure survey, temperature recovery, and general nozzle characteristics are provided.
Date:
October 25, 1949
Creator:
McLellan, Charles H.; Williams, Thomas W. & Bertram, Mitchel H.
System:
The UNT Digital Library