A control-volume method for analysis of unsteady thrust augmenting ejector flows
By: Colin K. Drummond.
Contributors: Lewis Research Center.
Series: NASA contractor report -- 182203.; NASA contractor report -- NASA CR-182203.
Publisher: Lewis Research Center, National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1988
Place of publication: Cleveland, Ohio; [Springfield, Va
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Computerized simulation.; Ejectors.; Finite volume method.; Mathematical models.; Thrust augmentation.; Turbulent jets.; Unsteady flow.
Other titles: Control volume method for analysis of unsteady thrust augmenting ejector flows.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 2 microfiches.