The Effect of Three-Dimensional Freestream Disturbances on the Supersonic Flow Past a Wedge by National Aeronautics and Space Adm Nasa

The Effect of Three-Dimensional Freestream Disturbances on the Supersonic Flow Past a Wedge

National Aeronautics and Space Adm Nasa

34 pages missing pub info (editions)

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The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional disturbances of a uniform, supersonic, freestream flow are investigated. The paper extends the two-dimensional study of Duck et al, through the use o...

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