James David Heidmann

The effect of wake passing on turbine blade film cooling

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Author

James David Heidmann

Contributions

United States. National Aeronautics and Space Administration. - Contributor

Publication

1996 - National Aeronautics and Space Administration, Washington, DC, District of Columbia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

Open LibraryOL15497548M

Subjects

Topics

Wakes Film cooling Turbomachinery Turbine blades Flow distribution Unsteady aerodynamics Navier-Stokes equation

Series Statement

NASA technical memorandum -- 107380.

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