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Howling of a Model-scale Nozzle Due to Shock-induced Boundary-layer Separation at its Exit

Ramsey, D. N., Gavin, J. R., & Ahuja, K. K. (2025). Howling of a model-scale nozzle due to shock-induced boundary-layer separation at its exit. Journal of Fluid Mechanics, 1014, A8. doi:10.1017/jfm.2025.10170

Participants

  • Georgia Institute of Technology

Projects

  • Jet Noise Modeling and Measurements to Support Reduced LTO Noise of Supersonic Aircraft Technology Development

Lead Investigators

  • Krishan Ahuja

    FAA Center of Excellence for Alternative Jet Fuels & Environment

    • Washington State University
    • Massachusetts Institute of Technology
    • Federal Aviation Administration
    © Washington State University