Validation of Computational Fluid Dynamics for supersonic Shock containing jets

Steven A.E. Miller, Jérémy Veltin, Philip John Morris, Dennis K. McLaughlin

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Citations (Scopus)

Abstract

This paper consists of an evaluation of Computational Fluid Dynamic (CFD) simulations for supersonic jets operating off-design with corresponding experiments. It is part of an ongoing project to predict Broadband Shock Associated Noise (BBSAN). Axisymmetric steady state CFD results are produced with a Reynolds Averaged Navier-Stokes solver using a two equation turbulence model. These results are directly compared with experimental results for two different axisymmetric nozzles operating over- and under-expanded. Profiles of Pitot pressure and static pressure probes form the basis for evaluating Mach number and local static pressure at various downstream locations. Both experimental and numerical schlieren are compared side by side for a qualitative assessment of the accuracy of the flowfield predictions. Numerical and experimental contour plots are produced for further analysis. Finally, CFD results are verified further by demonstrating how the shock noise source strength varies with the off-design parameter in preparation for the BBSAN model development.

Original languageEnglish (US)
Title of host publication14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
StatePublished - Dec 1 2008
Event14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) - Vancouver, BC, Canada
Duration: May 5 2008May 7 2008

Publication series

Name14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)

Other

Other14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
CountryCanada
CityVancouver, BC
Period5/5/085/7/08

Fingerprint

Computational fluid dynamics
Turbulence models
Mach number
Nozzles
Computer simulation
Experiments

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Miller, S. A. E., Veltin, J., Morris, P. J., & McLaughlin, D. K. (2008). Validation of Computational Fluid Dynamics for supersonic Shock containing jets. In 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) [2008-2988] (14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)).
Miller, Steven A.E. ; Veltin, Jérémy ; Morris, Philip John ; McLaughlin, Dennis K. / Validation of Computational Fluid Dynamics for supersonic Shock containing jets. 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference). 2008. (14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)).
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Miller, SAE, Veltin, J, Morris, PJ & McLaughlin, DK 2008, Validation of Computational Fluid Dynamics for supersonic Shock containing jets. in 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)., 2008-2988, 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), Vancouver, BC, Canada, 5/5/08.

Validation of Computational Fluid Dynamics for supersonic Shock containing jets. / Miller, Steven A.E.; Veltin, Jérémy; Morris, Philip John; McLaughlin, Dennis K.

14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference). 2008. 2008-2988 (14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Miller SAE, Veltin J, Morris PJ, McLaughlin DK. Validation of Computational Fluid Dynamics for supersonic Shock containing jets. In 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference). 2008. 2008-2988. (14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)).