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Book Chapter

Experimental and numerical investigation on the supersonic inlet buzz with angle of attack

  • Lee H
  • Jeung I
Springer Berlin Heidelberg, (2009), 1111-1116
DOI: 10.1007/978-3-540-85181-3_51
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Abstract

During inlet buzz, supersonic inlets exhibit considerable oscillation of the shock system in front of the inlet and corresponding large pressure fluctuations downstream. Inlet buzz is highly undesirable because of the decrease in efficiency or the total failure of...

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Lee, H.-J., & Jeung, I.-S. (2009). Experimental and numerical investigation on the supersonic inlet buzz with angle of attack. In Shock Waves (pp. 1111–1116). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_51

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