X-59 Sonic Boom Test Results from the NASA Glenn 8- by 6-Foot Supersonic Wind Tunnel

A wind tunnel test was conducted to investigate near-field sonic boom pressure signatures of the X-59 Low-Boom Flight Demonstrator aircraft. A 1.62%-scale model of the aircraft was fabricated for the wind tunnel test, which took place in the NASA Glenn 8- by 6-Foot Supersonic Wind Tunnel in Septembe...

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Bibliographische Detailangaben

Hauptverfasser:	Durston, Donald A, Wolter, John D, Shea, Patrick R, Winski, Courtney S, Elmiligui, Alaa A, Langston, Sarah L, Bozeman, Michael D, Carter, Melissa B, Bellido, Christopher A
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics
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