Numerical Investigation of a Supersonic Wind Tunnel Diffuser Optimization

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...

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Bibliographic Details
Main Authors: Riccardo Nicoletti, Francesco Margani, Luca Armani, Antonella Ingenito, Chihiro Fujio, Hideaki Ogawa, Seoeum Han, Bok Jik Lee
Format: Article
Language:English
Published: MDPI AG 2025-04-01
Series:Aerospace
Subjects:
supersonic wind tunnel
blowdown wind tunnel
CFD
second throat optimization
nozzle design
hypersonic
Online Access:https://www.mdpi.com/2226-4310/12/5/366
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