Large-eddy simulation of crackle in heated supersonic jets

ORAL

Abstract

Crackle noise from heated supersonic jets is characterized by the presence of strong positive pressure impulses resulting in a strongly skewed far-field pressure signal (Ffowcs Williams et al., 1975). These strong positive pressure impulses are associated with N-shaped waveforms involving a shock-like compression, and thus is very annoying to observers when it occurs. In this talk, the origins of these N-shaped waveforms is investigated through high-fidelity large-eddy simulations (LES) applied to an over-expanded supersonic jet issuing from a faceted military-style nozzle. Two different levels of heating are considered. From the LES, we observe N-shaped waves associated with crackle to emerge directly from the jet turbulence. Furthermore, even at this extreme near-field location, we find that the emergent waves are already well-organized, having correlation over significant azimuthal distances.

*Computational resources were provided by a DoD HPCMP Challenge Project allocation at the ERDC and AFRL supercomputing centers.

Authors

  • Joseph Nichols

    • Center for Turbulence Research (CTR), Stanford
    • Stanford University
    • Stanford University, Stanford, CA
  • Sanjiva K. Lele

    • Stanford University, Stanford, CA
  • Frank E. Ham

    • Cascade Technologies, Inc., Palo Alto, CA
  • Steve Martens

    • GE Global Research, Niskayuna, NY
  • John T. Spyropoulos

    • Naval Air Systems Command, Patuxent River, MD