A parallel implementation of a computational aeroacoustic algorithm for airfoil noise

David P. Lockard, Philip John Morris

Research output: Contribution to conferencePaper

9 Scopus citations

Abstract

The long-term objective of the research described in this paper is to use CAA methodology and parallel computers to increase the understanding of broadband blade noise. In a systematic progression towards simulations of completely realistic configurations and conditions, some simplified problems that address the important features of the flow are investigated. A two-dimensional, Navier-Stokes code, implemented using the message passing library and Fortran 90 on the IBM SP2, is used to perform the calculations. Results are presented for the interaction of a vortical gust and a flat plate.

Original languageEnglish (US)
DOIs
StatePublished - Jan 1 1996
Event2nd AIAA/CEAS Aeroacoustics Conference, 1996 - State College, United States
Duration: May 6 1996May 8 1996

Other

Other2nd AIAA/CEAS Aeroacoustics Conference, 1996
CountryUnited States
CityState College
Period5/6/965/8/96

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering
  • Aerospace Engineering

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    Lockard, D. P., & Morris, P. J. (1996). A parallel implementation of a computational aeroacoustic algorithm for airfoil noise. Paper presented at 2nd AIAA/CEAS Aeroacoustics Conference, 1996, State College, United States. https://doi.org/10.2514/6.1996-1754