Width effects in transonic flow over a rectangular cavity
- Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
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.
- Research Organization:
- Sandia National Laboratories (SNL-NM), Albuquerque, NM (United States)
- Sponsoring Organization:
- USDOE National Nuclear Security Administration (NNSA)
- Grant/Contract Number:
- AC04-94AL85000
- OSTI ID:
- 1237473
- Report Number(s):
- SAND--2015-2747J; 582041
- Journal Information:
- AIAA Journal, Journal Name: AIAA Journal Journal Issue: 12 Vol. 53; ISSN 0001-1452
- Publisher:
- AIAACopyright Statement
- Country of Publication:
- United States
- Language:
- English
Similar Records
Compressibility effects in the shear layer over a rectangular cavity
Spatial Distribution of Resonance in the Velocity Field for Transonic Flow over a Rectangular Cavity
Fluid-structure interactions in compressible cavity flows
Conference
·
Wed Oct 26 00:00:00 EDT 2016
· Journal of Fluid Mechanics
·
OSTI ID:1338675
Spatial Distribution of Resonance in the Velocity Field for Transonic Flow over a Rectangular Cavity
Journal Article
·
Thu Jul 27 00:00:00 EDT 2017
· AIAA Journal
·
OSTI ID:1399504
Fluid-structure interactions in compressible cavity flows
Journal Article
·
Mon Jun 08 00:00:00 EDT 2015
· Physics of Fluids
·
OSTI ID:1184573