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

Bibliographic Details

Main Authors:	Hussaini, M. Moin (Author), Korte, John J. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
Series:	NASA technical memorandum ; 110295.
Subjects:	Computational fluid dynamics. Navier-Stokes equation. Nozzle design. Rocket nozzles. Low Reynolds number. Nozzle thrust coefficients.
Online Access:	https://purl.fdlp.gov/GPO/LPS67205