Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer [ NASA TM X-3134]
Contributor(s): Blaha,Ronald. J. and Seldner, Kurt.
Material type:
BookSeries: National Aeronaticsand Space Administration (NASA). Publisher: Washington D.C. National Aeronaticsand Space Administration 1975Description: 34p.
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