A PRELIMINARY STUDY ON TRANSONIC SHOCK TUBE AIRFOIL FLOWS WITH TRANSFORMING GURNEY FLAP BY UTILIZING PDI

A PRELIMINARY STUDY ON TRANSONIC SHOCK TUBE AIRFOIL FLOWS WITH TRANSFORMING GURNEY FLAP BY UTILIZING PDI

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Ground testing
1. Verfasser: Kashitani, Masashi (VerfasserIn)
Weitere Verfasser: Taguchi, Masato (VerfasserIn), Duong, Nguyen T. (VerfasserIn), Oomori, Akinori (VerfasserIn), Nishiyama, Masanori (VerfasserIn), Tanno, Hideyuki (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2020
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