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Title: Width effects in transonic flow over a rectangular cavity

Abstract

A previous experiment by the present authors studied the flow over a finite-width rectangular cavity at freestream Mach numbers 1.5–2.5. In addition, this investigation considered the influence of three-dimensional geometry that is not replicated by simplified cavities that extend across the entire wind-tunnel test section. The latter configurations have the attraction of easy optical access into the depths of the cavity, but they do not reproduce effects upon the turbulent structures and acoustic modes due to the length-to-width ratio, which is becoming recognized as an important parameter describing the nature of the flow within narrower cavities.

Authors:
 [1];  [1];  [1];  [1];  [1]
  1. Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
Publication Date:
Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
Sponsoring Org.:
USDOE National Nuclear Security Administration (NNSA)
OSTI Identifier:
1237473
Report Number(s):
SAND-2015-2747J
Journal ID: ISSN 0001-1452; 582041
Grant/Contract Number:  
AC04-94AL85000
Resource Type:
Accepted Manuscript
Journal Name:
AIAA Journal
Additional Journal Information:
Journal Volume: 53; Journal Issue: 12; Journal ID: ISSN 0001-1452
Publisher:
AIAA
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Beresh, Steven J., Wagner, Justin L., Henfling, John F., Spillers, Russell Wayne, and Pruett, Brian Owen Matthew. Width effects in transonic flow over a rectangular cavity. United States: N. p., 2015. Web. doi:10.2514/1.J054362.
Beresh, Steven J., Wagner, Justin L., Henfling, John F., Spillers, Russell Wayne, & Pruett, Brian Owen Matthew. Width effects in transonic flow over a rectangular cavity. United States. https://doi.org/10.2514/1.J054362
Beresh, Steven J., Wagner, Justin L., Henfling, John F., Spillers, Russell Wayne, and Pruett, Brian Owen Matthew. Fri . "Width effects in transonic flow over a rectangular cavity". United States. https://doi.org/10.2514/1.J054362. https://www.osti.gov/servlets/purl/1237473.
@article{osti_1237473,
title = {Width effects in transonic flow over a rectangular cavity},
author = {Beresh, Steven J. and Wagner, Justin L. and Henfling, John F. and Spillers, Russell Wayne and Pruett, Brian Owen Matthew},
abstractNote = {A previous experiment by the present authors studied the flow over a finite-width rectangular cavity at freestream Mach numbers 1.5–2.5. In addition, this investigation considered the influence of three-dimensional geometry that is not replicated by simplified cavities that extend across the entire wind-tunnel test section. The latter configurations have the attraction of easy optical access into the depths of the cavity, but they do not reproduce effects upon the turbulent structures and acoustic modes due to the length-to-width ratio, which is becoming recognized as an important parameter describing the nature of the flow within narrower cavities.},
doi = {10.2514/1.J054362},
journal = {AIAA Journal},
number = 12,
volume = 53,
place = {United States},
year = {Fri Jul 24 00:00:00 EDT 2015},
month = {Fri Jul 24 00:00:00 EDT 2015}
}

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Cited by: 13 works
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Works referenced in this record:

Supersonic Flow over a Finite-Width Rectangular Cavity
journal, February 2015

  • Beresh, Steven J.; Wagner, Justin L.; Pruett, Brian O. M.
  • AIAA Journal, Vol. 53, Issue 2
  • DOI: 10.2514/1.J053097

Three-dimensional flow in cavities
journal, August 1963


Three-dimensional effect on transonic rectangular cavity flows
journal, May 2001


Three-dimensional centrifugal instabilities development inside a parallelepipedic open cavity of various shape
journal, May 2009

  • Faure, Thierry M.; Pastur, Luc; Lusseyran, François
  • Experiments in Fluids, Vol. 47, Issue 3
  • DOI: 10.1007/s00348-009-0671-0

Effect of finite cavity width on flow oscillation in a low-Mach-number cavity flow
journal, June 2011


Experimental Investigation of Aspect-Ratio Effects in Transonic Rectangular Cavity Flows
conference, January 2014

  • Wagner, Justin L.; Beresh, Steven J.; Casper, Katya M.
  • 52nd Aerospace Sciences Meeting
  • DOI: 10.2514/6.2014-1446

Works referencing / citing this record:

Self-calibration performance in stereoscopic PIV acquired in a transonic wind tunnel
journal, March 2016

  • Beresh, Steven J.; Wagner, Justin L.; Smith, Barton L.
  • Experiments in Fluids, Vol. 57, Issue 4
  • DOI: 10.1007/s00348-016-2131-y

Resonance dynamics in compressible cavity flows using time-resolved velocity and surface pressure fields
journal, October 2017

  • Wagner, Justin L.; Beresh, Steven J.; Casper, Katya M.
  • Journal of Fluid Mechanics, Vol. 830
  • DOI: 10.1017/jfm.2017.606

Spatial distribution of pressure resonance in compressible cavity flow
journal, June 2018

  • Casper, Katya M.; Wagner, Justin L.; Beresh, Steven J.
  • Journal of Fluid Mechanics, Vol. 848
  • DOI: 10.1017/jfm.2018.346

Fluid–Structure Interactions on a Tunable Store in Complex Cavity Flow
journal, July 2019

  • Casper, Katya M.; Wagner, Justin L.; Beresh, Steven J.
  • Journal of Aircraft, Vol. 56, Issue 4
  • DOI: 10.2514/1.c035050

Volumetric Velocimetry of Complex Geometry Effects on Transonic Flow over Cavities
journal, May 2019

  • DeMauro, Edward P.; Beresh, Steven J.; Casper, Katya M.
  • AIAA Journal, Vol. 57, Issue 5
  • DOI: 10.2514/1.j057714

Response of a Store with Tunable Natural Frequencies in Compressible Cavity Flow
conference, January 2015

  • Wagner, Justin L.; Casper, Katya M.; Beresh, Steven J.
  • 53rd AIAA Aerospace Sciences Meeting
  • DOI: 10.2514/6.2015-1293

Spatial Distribution of Pressure Resonance in Compressible Cavity Flow
conference, January 2017

  • Casper, Katya M.; Wagner, Justin L.; Beresh, Steven J.
  • 55th AIAA Aerospace Sciences Meeting
  • DOI: 10.2514/6.2017-1476