Behaviour of hypersonic wind tunnels diffusers at low Reynolds numbers-Reference-Cited by-同舟云学术

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Behaviour of hypersonic wind tunnels diffusers at low Reynolds numbers

Published:1999-01 Issue:1 Volume:3 Page:11-19
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Savino R.,Monti R.,Esposito A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference9 articles.

1. An experimental study of diffusers in an open jet, low density, hypersonic wind tunnel;Boylan,1964

2. The atmospheric reentry simulator in Naples;Esposito,1996

3. Supersonic wind tunnel diffuser performances with high model blockage at moderate to low Reynolds number;Hanus;AIAA paper 91-2274,1991

4. Study of a family of diffusers for low Reynolds number hypersonic wind tunnels;Monnerie;Rech. Aerospatiale,1966

5. Recent developments of the arc- heated flow facility in Naples;Monti,1997

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Investigation of Diffusers in Arc-Heated Wind Tunnel: Introducing a Novel and Efficient Hypersonic Diffuser;Journal of Aerospace Engineering;2022-09

2. Efficient diffuser design for plasma wind tunnels with a large blockage model;Aerospace Science and Technology;2021-12

3. Investigation of Hypersonic Flow in the VKI H3 Wind Tunnel: from Facility Characterization to Boundary-Layer Interaction over Low-Temperature Ablators;23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2020-03-10

4. Aerothermodynamic analyses and redesign of GHIBLI Plasma Wind Tunnel hypersonic diffuser;Aerospace Science and Technology;2019-04

5. Numerical Analysis of an Actively Cooled Low-Reynolds-Number Hypersonic Diffuser;Journal of Thermophysics and Heat Transfer;2019-01

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