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....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.Read More
Publication Year: 1977
Publication Date: 1977-12-01
Language: en
Type: article
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