A computational study of the flow in a transonic axial compressor using an inviscid, three-dimensional finite difference

May 1979

Bibliographic Details
Main Author:	Haymann-Haber, Guido
Other Authors:	Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory
Format:	Technical Report
Published:	Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1979] 2016
Subjects:	TJ778.M41 G24 no.145 Compressors > Aerodynamics Aerodynamics, Transonic
Online Access:	http://hdl.handle.net/1721.1/104422

Internet

http://hdl.handle.net/1721.1/104422