Department of Mechanical and Aerospace Engineering Reports 1947-1998

• A detailed study of the interaction of a 14 degree shock wave with a turbulent boundary layer at m=2.9 Call Number: ENG007_c0122
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• A detailed study of the interaction of a 14 degree shock wave with a turbulent boundary layer at m=2.9

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A detailed study of the interaction of a 14 degree shock wave with a turbulent boundary layer at m=2.9

1 item

This collection is stored at Engineering Library.

Material may be viewed at Technical and Scientific Reports, Engineering Library Reading Room .

Identifier: Report no. 296

Creator: Vas, I.E..

Collection Creator: Princeton University. Dept. of Mechanical and Aerospace Engineering..

Dates: 1955 April.

Extent: 1 item

Languages: English.

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Preferred Citation

A detailed study of the interaction of a 14 degree shock wave with a turbulent boundary layer at m=2.9; 1955 April; Department of Mechanical and Aerospace Engineering Reports, Technical and Scientific Reports, Engineering Library, Princeton University Library.