Investigation of Hypersonic Flow in the VKI H3 Wind Tunnel: from Facility Characterization to Boundary-Layer Interaction over Low-Temperature Ablators-Reference-Cited by-同舟云学术

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Investigation of Hypersonic Flow in the VKI H3 Wind Tunnel: from Facility Characterization to Boundary-Layer Interaction over Low-Temperature Ablators

Published:2020-03-10 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Agostinelli Pasquale Walter¹,Turchi Alessandro²,Le Quang Damien²,Masutti Davide²,Vigevano Luigi¹,D'Ambrosio Domenic³,Chazot Olivier²

Affiliation:

1. Technical University of Milan

2. von Kármán Institute for Fluid Dynamics

3. Technical University of Turin

Publisher

American Institute of Aeronautics and Astronautics

Reference42 articles.

1. AndersonJr,J.D.,Hypersonicandhigh-temperaturegasdynamics,AmericanInstituteofAeronauticsandAstronautics,2006.

2. Turchi,A.“ModellingCapsuleStabilityAccountingforShapeChange.Technical,Implementation,ManagementandFinancial Proposal,”Tech.rep.,VonKarmanInstituteforFluidDynamics,2017.

3. Pope,A.,andGoin,K.“High-speedWindTunnelTesting,”,1978.

4. Wind tunnel facility calibrations and experimental uncertainty

Cited by 1 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. Renewed characterization of a Mach 6 hypersonic wind tunnel;AIAA SCITECH 2023 Forum;2023-01-19

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