A final report on NASA grant NSG 3079 entitled A linearized Euler analysis of unsteady flows in turbomachinery
By: by Kenneth C. Hall and Edward F. Crawley.
Contributors: Crawley, Edward F.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-180987.
Publisher: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1987
Place of publication: Cambridge, MA; [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Cascade flow.; Computational fluid dynamics.; Eular equations of motion.; Linearization.; Shock waves.; Turbine blades.; Turbomachinery.; Unsteady flow.
Other titles: Linearized Euler analysis of unsteady flows in turbomachinery.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1987] 2 microfiches.