Art
J-GLOBAL ID:201902217490940128   Reference number:19S1734600

Numerical study of flow angles and mach number measurement using the surface pressure of a supersonic aircraft with nose cone

Author (3):
Material:
Volume: 55  Issue:Page: 81-88  Publication year: 2012 
JST Material Number: SCOPUS  ISSN: 0549-3811  CODEN: TJASA 
Country of issue: Japan (JPN)  Language: English (EN)

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