FORTRAN program for calculating three-dimensional, inviscid, rotational flows with shock waves in axial compressor blade rows
Subtitle: user's manual
By: William T. Thompkins ; prepared for Lewis Research Center under grant NSG-3234
Contributors: Lewis Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory
Series: NASA contractor report -- 3560
Publisher: National Aeronautical and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 170
Subjects: Turbomachines; Lagrange equations; Compressors -- Aerodynamics
Notes: "Massachusetts Institute of Technology, Gas Turbine and Plasma Dynamics Laboratory"--Tech. rep. p

STAR category 02

"June 1982"--Cover

Includes bibliographical references