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

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

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