Three-dimensional effect on transonic rectangular cavity flows

Experiments in Fluids

Volumn 30, Issue 5, 2001, Pages 531-536

  Chung, K M ^a  

^a NATIONAL CHENG KUNG UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; DATA ACQUISITION; PRESSURE DISTRIBUTION; PRESSURE TRANSDUCERS; REYNOLDS NUMBER; SHOCK WAVES; SUPERSONIC FLOW; WIND TUNNELS;

TRANSONIC RECTANGULAR CAVITY FLOWS;

TRANSONIC FLOW;

EID: 0035327545     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003480000232     Document Type: Article

References (13)

1. Computational and experimental investigation of cavity flow fields
2. Estimation of possible excitation frequencies for shallow rectangular cavities
3. Development and calibration of ASTRC/NCKU 600 mm × 600 mm transonic wind tunnel
4. Resolution of pressure in turbulence
5. A review of knowledge on pressure fluctuations
6. Navier-Stokes study of supersonic cavity flow field with passive control
7. Prediction and measurement of flows over cavities - A survey
8. Prediction of oscillation frequencies for unstable flow past cavities
9. Review-self sustaining oscillations of flow past cavities
10. Experimental cavity pressure distributions at supersonic speeds
11. Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers
12. An investigation of supersonic cavity flows driven by thick shear layers