An integral equation solution for multi-stage turbomachinery design calculations
By: Eric R. McFarland.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 105970.; NASA technical memorandum -- 105970.
Publisher: National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1993
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Turbomachines -- Blades.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-0436-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 1 microfiche.