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Computational and Experimental Study of Plume and Shock Interaction Effects on Sonic Boom in the NASA Ames 9x7 Supersonic Wind Tunnel
Author(s) -
Courtney S. Winski,
Melissa B. Carter,
Alaa Elmiligui,
Jason M. Pearl,
Sudheer N. Nayani,
Donald A. Durston
Publication year - 2018
Publication title -
2018 aiaa aerospace sciences meeting
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2018-0331
Subject(s) - supersonic wind tunnel , sonic boom , wind tunnel , nozzle , shock wave , supersonic speed , plume , schlieren photography , aerospace engineering , aerodynamics , schlieren , mach number , shock (circulatory) , hypersonic wind tunnel , marine engineering , shock diamond , computational fluid dynamics , engineering , bow shock (aerodynamics) , mechanics , meteorology , flow (mathematics) , flow visualization , physics , medicine

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