Experimental determination of the free-stream disturbance field in a short-duration supersonic wind tunnel-Reference-Cited by-同舟云学术

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Experimental determination of the free-stream disturbance field in a short-duration supersonic wind tunnel

Published:2003-10-01 Issue:4 Volume:35 Page:291-302
ISSN:0723-4864
Container-title:Experiments in Fluids
language:
Short-container-title:Experiments in Fluids

Author:

Weiss J.,Knauss H.,Wagner S.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1007/s00348-003-0623-z.pdf

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1. Mode decomposition of disturbances in a supersonic flow;Thermophysics and Aeromechanics;2020-09

2. Characterization of a Ludwieg Tube with Free Piston Compression Heating in Mach 6 Configuration;22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference;2018-09-15

3. Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer;AIP Conference Proceedings;2018

4. Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability;AIP Conference Proceedings;2018

5. Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer;AIP Conference Proceedings;2018

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