Calculation of multistage turbomachinery using steady characteristic boundary conditions
By: Rodrick V. Chima.
Contributors: Langely Research Center.
Series: NASA/TM -- 206613.; NASA technical memorandum -- 206613.
Publisher: National Aeronautics and Space Administration Langley Research Center; Available from National Technical Information Service
Published: 1998
Place of publication: [Cleveland, Ohio]; Springfield, Va
Language: eng
Format: Microform
Notes: Shipping list no.: 98-0087-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.