Effects of dual jets distance on mixing characteristics and flow path within a cavity in supersonic crossflow
Creators
- 1. Institute of Fluid Science, Tohoku University, 2-1-1 Katahira, Aoba-ku, Sendai, Miyagi 980-8577 (Japan)
- 2. School of Engineering, University of Glasgow, Scotland G12 8QQ (United Kingdom)
Description
Highlights: • The enhancement of air mixing depends on the distance between the jets. • The long dual jets distance is better than short one for the mixing. • The mixing is enhanced within the cavity by effects of the opposed flow. • Mainstream between two vortex pairs behind the jets flows strongly into the cavity. • The unstable flow occurs over the cavity at the long and short dual jets distance. - Abstract: A rectangular open cavity with upstream dual injectors at a freestream Mach number of 1.9 was investigated experimentally. To evaluate the effect of the distance between the jets, the flow characteristics were investigated using the high-speed schlieren photography, particle image velocimetry, and surface oil flow techniques. The dual jet distances of 18 and 54 mm were used. Unstable flow occurs over the cavity in all cases and is not improved by changing the distance between the dual jets. Although the distance between the dual jets does not influence the flow stability, the flow field varies decidedly depending on the dual jets distance. The enhancement of air mixing depends on the distance between the jets. A long dual jets distance was found to yield better mixing characteristics within the cavity than a short one. When the jets are further apart, the mainstream between two counter-rotating vortex pairs behind the jets flows strongly into the cavity because of the increased blow-down occurring between the vortex pairs. Additionally, a counterflow with a low velocity magnitude occurs behind the jets. Hence, mixing is enhanced within the cavity by effects of the opposed flow. When the jet pairs are closer to each other, the counter-rotating vortex pairs are in contact; as a result, the blow-down effect does not occur between them. The flow drawn into the cavity from the mainstream is supplied from the sides of the test section into the cavity
Availability note (English)
Available from http://dx.doi.org/10.1016/j.ijheatfluidflow.2014.08.009Additional details
Identifiers
- DOI
- 10.1016/j.ijheatfluidflow.2014.08.009;
- PII
- S0142-727X(14)00102-7;
Publishing Information
- Journal Title
- International Journal of Heat and Fluid Flow
- Journal Volume
- 50
- Journal Page Range
- p. 254-262
- ISSN
- 0142-727X
- CODEN
- IJHFD2
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 47007780
- Subject category
- S42: ENGINEERING;
- Descriptors DEI
- AIR; CAVITIES; DISTANCE; IMAGES; JETS; MACH NUMBER; MIXING; OILS; PHOTOGRAPHY; SUPERSONIC FLOW; VORTICES
- Descriptors DEC
- DIMENSIONLESS NUMBERS; FLUID FLOW; FLUIDS; GASES; ORGANIC COMPOUNDS; OTHER ORGANIC COMPOUNDS; VELOCITY
Optional Information
- Copyright
- Copyright (c) 2014 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.