Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure /

Bibliographic Details

Main Author:	Hussaini, M. Moin
Corporate Author:	Langley Research Center
Other Authors:	Korte, John J.
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [1996]
Series:	NASA technical memorandum ; 110295.
Subjects:	Computational fluid dynamics. Navier-Stokes equation. Nozzle design. Rocket nozzles. Low Reynolds number. Nozzle thrust coefficients.