Shock Structure in Transonic Compressor Rotors
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61134
Reference4 articles.
1. Quantitative Density Visualization in a Transonic Compressor Rotor
2. 2Thompkins, Jr., W. T. "An Experimental and Computational Study of the Flow in a Transonic Compressor Rotor," Ph.D. Thesis,Massachusetts Institute of Technology, June 1976; also M.I.T. Gas Turbine Lab. Rept. No. 129, May 1976.
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