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Some special features of the flow in compressed layer downstream the incident shock in overexpanded jet

  • Uskov V
  • Chernyshov M
Springer Berlin Heidelberg, (2009), 1509-1514
DOI: 10.1007/978-3-540-85181-3_116
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Abstract

The mathematical model for the investigation of two-dimensional overexpanded jet flow parameters in the vicinity of supersonic nozzle edge is formulated. The variation of the key parameter of this problem (i.e., the geometrical curvature of the shock emanating from the nozzle lip) is studied depending on flow conditions.

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Uskov, V. N., & Chernyshov, M. V. (2009). Some special features of the flow in compressed layer downstream the incident shock in overexpanded jet. In Shock Waves (pp. 1509–1514). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_116

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