Richard J. Re

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

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Author

Richard J. Re

Contributions

Abeyounis, William Kelly. - Contributor
Langley Research Center. - Contributor

Publication

1996 - National Aeronautics and Space Administration, Langley Research Center, Hampton, Va, Virginia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

Open LibraryOL15498125M

Subjects

Topics

Mach number Engine inlets Subsonic flow Angle of attack Static pressure Aircraft engines Wind tunnel tests

Series Statement

NASA technical memorandum -- 110300.

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