Crawford F. Smith

Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack

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Author

Crawford F. Smith

Contributions

United States. National Aeronautics and Space Administration. - Contributor

Publication

1995 - National Aeronautics and Space Administration, Washington, D.C., District of Columbia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

Open LibraryOL15409179M

Subjects

Topics

Air flow Inlet flow Wind tunnels Engine inlets F-18 aircraft Intake systems Angle of attack

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