Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts /

Bibliographic Details
Main Author:	Anderson, O. L. (Olos Lennart), 1931-
Corporate Authors:	United Aircraft Corporation, Lewis Research Center
Format:	Book
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration ; 1974.
Series:	NASA contractor report ; NASA CR-2365.
Subjects:	Diffusers > Aerodynamics > Computer simulation. Turbulence. Finite differences.

Description
Item Description:	Cover title. "Prepared by United Aircraft Corporation ... for Lewis Research Center."
Physical Description:	iv, 149 pages : illustrations ; 27 cm.
Bibliography:	Bibliography: pages 59-60.