Rodrick V. Chima

Calculation of multistage turbomachinery using steady characteristic boundary conditions

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Author

Rodrick V. Chima

Contributions

Langely Research Center. - Contributor

Publication

1998 - National Aeronautics and Space Administration Langley Research Center, Cleveland, Ohio, District of Columbia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

OCLC Control Number41267349
Open LibraryOL17593118M

Subjects

Topics

Turbines Multiblock grids Turbulence models Pressure distribution Navier-Stokes equation Finite difference theory Heat transfer coefficients

Series Statement

NASA/TM -- 206613.
NASA technical memorandum -- 206613.

Other Editions

Calculation of multistage turbomachinery using steady characteristic boundary conditionsMicroformNational Aeronautics and Space Administration Langley Research Center1998-01-01

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