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Novel method for supersonic inlet buzz measurement in wind tunnel

Daliri, A ; Sharif University of Technology | 2018

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  1. Type of Document: Article
  2. DOI: 10.2514/1.B36760
  3. Publisher: American Institute of Aeronautics and Astronautics Inc , 2018
  4. Keywords:
  5. buzz phenomenon ; supersonic intake
  6. Source: Journal of Propulsion and Power ; Volume 34, Issue 1 , 2018 , Pages 273-277 ; 07484658 (ISSN)
  7. URL: https://arc.aiaa.org/doi/10.2514/1.B36760