Surface measurements of a supersonic jet in subsonic compressible crossflow

15th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2001, Pages

  Beresh, S J ^a   Henfling, J F ^a   Erven, R J ^a  

^a SANDIA NATIONAL LABORATORIES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLOW SEPARATION; NOZZLES; SURFACE MEASUREMENT;

COMPRESSIBLE CROSSFLOW; FREE-STREAM DYNAMIC PRESSURE; FREESTREAM MACH NUMBER; JET IN CROSSFLOW; SEPARATED FLOWS; STATIC PRESSURE; SUPERSONIC JETS; SURFACE PRESSURE FIELD;

SUPERSONIC AERODYNAMICS;

EID: 85088341717     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2786     Document Type: Conference Paper

References (41)

1. Chocinski, D., Leblanc, R., and Hachemin, J.-V., Experimental/Computational Investigation of Supersonic Jet in Subsonic Compressible Crossflow, AIAA Paper 97-0714, January 1997.
2. Chocinski, D., Contribution to the Modeling of Interactions of a Supersonic Jet in a Subsonic Compressible Crossflow, Doctoral Thesis, University of Poitiers, France, 1998.
3. Reichenau, D. E. A., Interference Effects Produced by a Cold Jet Issuing Normal to the Airstream from a Flat Plate, AEDC TR-67-220, October 1967.
4. Lee, E. E. Jr, and Willis, C. M., Interaction Effects of a Control Jet Exhausting Radially from the Nose of an Ogive-Cylinder Body at Transonic Speeds, NASA TN D-3752, January 1967.
5. Manela, J., and Seginer, A., Interaction of Multiple Supersonic Jets with a Transonic Flowfield, AIAA Journal Vol. 24, No. 3, 1986, pp. 418-423.
6. Kuiper, R. A., Control Jet Effectiveness in the Subsonic and Transonic Flight Regimes, Philco Aeronautic Division publication U-2932, December 1964.
7. Cassel, L. A., Durando, N. A., Bullard, C. W., and Kelso, J. M., Jet Interaction Control Effectiveness for Subsonic and Supersonic Flight, Report No. RD-TR- 69-21, U. S. Army Missile Command, Redstone Arsenal, September 1969.
8. Manela, J., and Seginer, A., Jet Penetration Height in Transonic Flow, AIAA Journal, Vol. 24, No. 1,1986, pp. 67-73.
9. Spring, D. J., An Experimental Investigation of the Interference Effects due to a Lateral Jet Issuing from a Body of Revolution over the Mach Number Range of 0.8 to 5, Report No. RD-TR-68-10, U.S. Army Missile Command, Redstone Arsenal, August 1968.
10. Dahlke, C. W., An Experimental Investigation of Downstream Flow-Field Properties Behind a Sonic Jet Injected into Transonic Free Stream from a Body of Revolution, Report No. RD-TR-69-2, U.S. Army Missile Command, Redstone Arsenal, February 1969.
11. Street, T. A., An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate into a Subsonic Free Stream, Report No. RD-TM-70-5, U.S. Army Missile Command, Redstone Arsenal, May 1970.
12. Shaw, C. S., and Margason, R. J., An Experimental Investigation of a Highly Underexpanded Sonic Jet Ejecting from a Flat Plate into a Subsonic Crossflow, NASA TN D-7314, December 1973.
13. Wang, K. C., Smith, O. I., and Karagozian, A. R., In-Flight Imaging of Transverse Gas Jets Injected into Compressible Crossflows, AIAA Journal, Vol. 33, No. 12, 1995, pp. 2259-2263.
14. Green, L. Jr., Flow Separation in Rocket Nozzles, ARS Journal, Vol. 23, No. 1, 1953, pp. 34-35.
15. Summerfield, M., Foster, C. R., and Swan, W. C., Flow Separation in Overexpanded Supersonic Exhaust Nozzles, Jet Propulsion, Vol. 24, Sep-Oct 1954, pp. 319-321.
16. Page, R. H., Flow Separation in Nozzles, Journal of the Aerospace Sciences, Vol. 29, Januiary 1962, pp. 110-111.
17. Schilling, M., Flow Separation in a Rocket Nozzle, M. S. Thesis, Graduate School of Arts and Sciences, University of Buffalo, Buffalo, NY, June 1962.
18. Arens, M., and Spiegler, E., Shock-Induced Boundary Layer Separation in Overexpanded Conical Exhaust Nozzles, AIAA Journal, Vol. 1, No. 3, 1963, pp. 578-581.
19. Chen, C. L., Chakravarthy, S. R., and Hung, C. M., Numerical Investigation of Separated Nozzle Flows, AIAA Journal, Vol. 32, No. 9, 1994, pp. 1836-1843.
20. Hamed, A., and Vogiatzis, C., Overexpanded Two-Dimensional Convergent-Divergent Nozzle Performance, Effects of Three-Dimensional Flow Interactions, Journal of Propulsion and Power, Vol. 14, No. 2, 1998, pp. 234-240.
21. Romine, G. L., Nozzle Flow Separation, AIAA Journal, Vol. 36, No. 9, 1998, pp. 1618-1625.
22. Hunter, C. A., Experimental, Theoretical, and Computational Investigation of Separated Nozzle Flows, AIAA Paper 98-3107, July 1998.
23. McKee, M. L., Digital Computer Oriented Methods for Determining the Response of Pressure Measurement to Step and Ramp Forcing Functions, AEDC Report TR-66-225, March 1967.
24. Shaw, R., The Influence of Hole Dimensions on Static Pressure Measurements, Journal of Fluid Mechanics, Vol. 7, 1960, pp 550-563.
25. Guy, R. W., and Winebarger, R. M., Effect of Orifice Size and Heat-Transfer Rate on Measured Static Pressures in a Low-Density Arc-Heated Wind Tunnel, NASA TN D-3829, February 1967.
26. Rainbird, W. J., Errors in Measurement of Mean Static Pressure of a Moving Fluid due to Pressure Holes, National Aeronautical Establishment Quarterly Bulletin, 1967, No. 3, pp 55-89.
27. Moulden, T. H., Wu, J. M., Collins, F. G., and Ramon, H. J., Experimental Study of Static Pressure Orifice Interference, AEDC TR 77-57, June 1977.
28. Ducruet, C., and Dyment, A., The Pressure-Hole Problem, Journal of Fluid Mechanics, Vol. 142, 1984, pp. 251-267.
29. Ducruet, C., A Method for Correcting Wall Pressure Measurements in Subsonic Compressible Flow, Transactions oftheASME, Vol. 113, June 1991, pp. 256-260.
30. Fric, T. F., and Roshko, A., Vortical Structure in the Wake of a Transverse Jet, Journal of Fluid Mechanics, Vol. 279, 1994, pp. 1-47.
31. Krothapalli, A., Lourenco, L., and Buchlin, J. M., Separated Flow Upstream of a Jet in a Crossflow, AIAA Journal, Vol. 28, No. 3, 1990, pp. 414-420.
32. Kelso, R. M., and Smits, A. J., Horseshoe Vortex Systems Resulting from the Interaction between a Laminar Boundary Layer and a Transverse Jet, Physics of Fluids, Vol. 7, No. 1, 1995, pp. 153-158.
33. Kelso, R. M., Lim, T. T., and Perry, A. E., An Experimental Study of Round Jets in Cross-flow, Journal of Fluid Mechanics, Vol. 306, 1996, pp. 111-144.
34. Sykes, R. I., Lewellen, W. S., and Parker, S. F., On the Vorticity Dynamics of a Turbulent Jet in a Crossflow, Journal of Fluid Mechanics, Vol. 168, 1986, pp. 393-413.
35. Yuan, L. L., Street, R. L., and Ferziger, J. H., Large-eddy Simulations of a Round Jet in Crossflow, Journal of Fluid Mechanics, Vol. 379, 1999, pp. 71-104.
36. Everett, D. E., Woodmansee, M. A., Dutton, J. C., and Morris, M. J., Wall Pressure Measurements for a Sonic Jet Injected Transversely into a Supersonic Crossflow, Journal of Propulsion and Power, Vol. 14, No. 6, 1998, pp. 861-868.
37. Gruber, M. R., and Goss, L. P., Surface pressure Measurements in Supersonic Transverse Injection Flowfields, Journal of Propulsion and Power, Vol. 15, No. 5, 1999, pp. 633-641.
38. Orth, R. C., and Funk, J. A., An Experimental and Comparative Study of Jet Penetration in Supersonic Flow, Journal of Spacecraft, Vol. 4, No. 9, 1967, pp. 1236-1242.
39. Kamotani, Y., and Greber, I., Experiments on a Turbulent Jet in a Cross Flow, AIAA Journal, Vol. 10, No. 11, 1972, pp. 1425-1429.
40. Papamoschou, D., and Hubbard, D. G., Visual Observations of Supersonic Transverse Jets, Experiments in Fluids, Vol. 14, 1993, pp. 468-471.
41. Margason, R. J., Fifty Years of Jet in Cross Flow Research, Computational and Experimental Assessment of Jets in Cross Flow, AGARD CP 534, 1993, pp. 1.1-1.41.