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Nozzle Plume/Shock Interaction Sonic Boom Test Results from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel
Nozzle Plume/Shock Interaction Sonic Boom Test Results from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel
2017
Donald A. Durston
Susan E. Cliff
Marie Denison
Derek J. Dalle
Raymond S. Castner
Alaa A. Elmiligui
Melissa B. Carter
Courtney S. Winski
Patrick R. Shea
Brennan T. Blumenthal
Nathanial T. Smith
Keywords:
Nozzle
Aeronautics
Plume
Supersonic wind tunnel
Sonic boom
Aerospace engineering
Engineering
Correction
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