Research Catalog

Title

Effect of fin leading edge sweep on shock-shock interaction at Mach 6 [microform] / Scott A. Berry and Robert J. Nowak.

Author

Berry, Scott A.

Publication

Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

Details

Additional Authors

• Nowak, Robert J.
• United States. National Aeronautics and Space Administration.

Description

1 v.

Series Statement

NASA technical memorandum ; 111790

Subject

• Leading edge sweep
• Shock wave interaction
• Wind tunnel tests
• Hypersonic speed
• Reynolds number

Note

• Shipping list no.: 98-0007-M.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:111790

OCLC

marcive41113148

Author

Berry, Scott A.

Title

Effect of fin leading edge sweep on shock-shock interaction at Mach 6 [microform] / Scott A. Berry and Robert J. Nowak.

Imprint

Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

Series

NASA technical memorandum ; 111790

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.

Added Author

Nowak, Robert J.

United States. National Aeronautics and Space Administration.

Report No.

AIAA-96-0230

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:111790

Research Call Number

READEX Microfiche NAS 1.15:111790