Axisymetric supersonic nozzle design foelsch method

Desai, SS (1977) Axisymetric supersonic nozzle design foelsch method. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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Abstract

A computer programme is given here for the calculation of13; axisymmetric supersonic nozzles for use in aerodynamic test13; facilities The approximate method due to Foelsch is adopted.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: calculation of axisymmetric supersonic nozzles;Aerodynamic test
Subjects: AERONAUTICS > Aerodynamics
Depositing User: M/S ICAST NAL
Date Deposited: 14 Sep 2006
Last Modified: 24 May 2010 04:20
URI: http://nal-ir.nal.res.in/id/eprint/2715

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