Numerical Investigation of a Supersonic Wind Tunnel Diffuser Optimization

The objective of this study is to enhance the methodology for the design of a supersonic wind tunnel, improving the process with advanced computational techniques. The supersonic wind tunnel is intended to operate within a flight envelope of Mach 2.5 to 4 and altitudes between 18 and 20 km; this stu...

詳細記述

書誌詳細

出版年:	Aerospace
主要な著者:	Riccardo Nicoletti, Francesco Margani, Luca Armani, Antonella Ingenito, Chihiro Fujio, Hideaki Ogawa, Seoeum Han, Bok Jik Lee
フォーマット:	論文
言語:	英語
出版事項:	MDPI AG 2025-04-01
主題:	supersonic wind tunnel blowdown wind tunnel CFD second throat optimization nozzle design hypersonic
オンライン･アクセス:	https://www.mdpi.com/2226-4310/12/5/366