Development of some hypersonic benchmark flows using CFD and experiment-Reference-Cited by-同舟云学术

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Development of some hypersonic benchmark flows using CFD and experiment

Published:2003-03-01 Issue:5 Volume:12 Page:375-384
ISSN:0938-1287
Container-title:Shock Waves
language:
Short-container-title:Shock Waves

Author:

Hillier R.,Boyce R.R.,Creighton S.A.,Fiala A.,Jackson A.P.,Mallinson S.G.,Sheikh A.H.,Soltani S.,Williams S.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/s00193-003-0179-0.pdf

Cited by 11 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. Grid independence in the study of boundary layer and its application in Hypergolic Propellants;International Journal of Precision Engineering and Manufacturing;2016-07

2. Expansion Tubes in Australia;Experimental Methods of Shock Wave Research;2015-11-01

3. The Performance Evaluation of an Improved Finite Volume Method for Solving the Navier Stokes Equation;53rd AIAA Aerospace Sciences Meeting;2015-01-03

4. Experimental investigation of axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions;Journal of Fluid Mechanics;2013-01-02

5. Simulation of High Mach Number Scramjet Flow Conditions using the X2 Expansion Tube;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

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