Rocket-based combined cycle engine technology development
Subtitle: inlet CFD validation and application
By: J.R. DeBonis and S. Yungster.
Contributors: Yungster, S.; Lewis Research Center. Institute for Computational Mechanics in Propulsion.
Series: NASA technical memorandum -- 107274.; ICOMP -- 96-6.
Publisher: National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion; National Aeronautics and Space Administration, distributor]
Published: 1996
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Rocket engine design.; Rocket engines.; Engine inlets.; Navier-Stokes equation.; Computational fluid dynamics.; Flow distribution.; Pressure distribution.; Static pressure.; Computational grids.; Hypersonic flow.
Other titles: Rocket based combined cycle engine technology development.
Notes: Shipping list no.: 98-0769-M.

Microfiche. [Washington, D.C.] : Supt. of Docs., U.S. G.P.O., [1997] 1 microfiches.