Flow distribution around the SSME main injector assembly using porosity formulation
By: Gary C. Cheng, Yen-Sen Chen, and Ten-See Wang.
Contributors: Chen, Yen-Sen.; Wang, Ten-See, 1950-; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA-CR-202070.; NASA contractor report -- NASA CR-202070.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Flow distribution.; Space Shuttle main engine.; Injectors.; Porosity.; Turbulent flow.; High temperature gases.; Reynolds number.; Drag.; Computational fluid dynamics.; Gas flow.; Navier-Stokes equation.
Notes: Shipping list no.: 98-0975-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.