Development of a turbomachinery design optimization procedure using a multiple-parameter nonlinear perturbation method
By: Stephen S. Stahara
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA contractor report -- 3831; NASA contractor report -- NASA CR-3831
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; National Technical Information Service, distributor]
Published: 1984
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Notes: Distributed to depository libraries in microfiche

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 3 microfiches