Effects of swirl and skew upon supersonic wall jet in crossflow

Journal of Propulsion and Power

Volumn 17, Issue 6, 2001, Pages 1327-1332

  Cutler, A D ^a   Doerner, S E ^a  

^a GEORGE WASHINGTON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FUEL INJECTION; GAS FUEL ANALYSIS; JETS; NOZZLES; PRESSURE; SWIRLING FLOW; WALL FLOW;

MACH NUMBER; MASS FLOW RATE; STATIC PRESSURE;

SUPERSONIC FLOW;

EID: 0035509678     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5882     Document Type: Article

References (16)

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2. Low angle injection into a supersonic flow
3. Gaseous injection in high speed flow
4. Mixing studies of helium in air at high supersonic speeds
5. Study of a supersonic combustor employing swept ramp fuel injectors
6. Near field flow of supersonic swirling jets
7. An experimental study of compressible turbulent mixing enhancement in swirling jets
8. Experiments on shock/vortex interaction
9. Mixing of swirling jets in a supersonic duct flow
10. Spin sail
11. Streamwise vortex production by pitched and skewed jets in a turbulent boundary layer
12. Flow and heat transfer in a turbulent boundary layer through skewed and pitched jets
13. Mixing enhancement by jet swirl in a multiport injector array in supersonic flow
14. Effects of jet swirl on mixing of a light gas jet in a supersonic airstream
15. Vortex flow in a convergent-divergent nozzle
16. Analysis of intermittency and probe data in a supersonic flow with injection