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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1988, Vol. 9 ›› Issue (2): 77-81.

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ENGINEERING METHOD FOR PREDICTING PRESSURE AND HEAT RATE OF THE COMPRESSIBLE CORNER REGION

Yang Maozhao   

  1. China Aerodynamic Research and Development Centre
  • Received:1988-01-14 Revised:1900-01-01 Online:1988-02-25 Published:1988-02-25

Abstract: An iterative correction method is presented in this paper for predicting the pressure and the heat rate in the separated and reattached regions in a compressible corner. The metho’d is constructed based on the basic separated flow patterns, in conjunction with empirical formulas. For the two-dimensional compressible corner, good agreement is obtained for the pressure and heat rate with the experimental data.