Experimental and Computational Study for the X-59 Wind Tunnel Model at Glenn Research Center 8- by 6-Foot Supersonic Wind Tunnel
AIAA Aviation Forum and Exposition ; 2023 ; San Diego, CA, US
Sonstige
Keine Angabe
Englisch
Aerodynamics , CST , X-59 , sonic boom , Low Boom , Quesst
AERODYNAMIC TESTING CAPABILITIES OF THE NASA GLENN 10- BY 10-FOOT SUPERSONIC WIND TUNNEL
British Library Conference Proceedings | 2011
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