Jet interaction with a primary jet and an array of smaller jets

AIAA Journal

Volumn 42, Issue 7, 2004, Pages 1358-1368

  Viti, Valerio ^a,d,e   Wallis, Scott ^a,f   Schetz, Joseph A ^a,d   Neel, Reece ^b,d   Bowersox, R D W ^c,g  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b AeroSoft Inc   (United States)

^c TEXAS A AND M UNIVERSITY   (United States)

^d Department of Aerospace Engineering ^*  (United States)

^e UNIVERSITY OF KENTUCKY   (United States)

^f SCIENCE APPLICATIONS INTERNATIONAL CORPORATION   (United States)

^g 3141 TAMU ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; INTEGRATION; NAVIER STOKES EQUATIONS; PLATES (STRUCTURAL COMPONENTS); TURBULENCE; TURBULENT FLOW; VECTORS; VISCOSITY;

CROSSFLOWS; INJECTORS; JET THRUSTERS; PRESSURE GRADIENTS;

JETS;

EID: 3342919247     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.4850     Document Type: Article

References (28)

1. "Computational and Experimental Assessment of Jets in Crossflow," Proceedings of the 72nd AGARD Fluid Dynamics Panel Meeting and Symposium, CP 534, AGARD, 1993.
2. Spaid, F. W., Zukoski, E. E., and Rosen, R., "A Study of Secondary Injection of Gases into a Supersonic Flow," NACA TR 32-834, Aug. 1966.
3. Schetz, J. A., Cox-Stouffer, S., and Fuller, R., "Integrated CFD and Experimental Studies of Complex Injectors in Supersonic Flows," AIAA Paper 98-2780, June 1998.
4. Schetz, J. A., Hawkins, P. F., and Lehman, H., "Structure of Highly Underexpanded Transverse Jets in a Supersonic Stream," AIAA Journal, Vol. 5, No. 5, 1967, pp. 882-884.
5. Cubbison, R. B., Anderson, B. H., and Ward, J. J., "Surface Pressure Distributions with a Sonic Jet Normal to Adjacent Flat Surfaces at Mach 2.92 to 6.4," NASA TN D-580, 1961.
6. Letko, W., "Loads Induced on a Flat Plate at a Mach Number of 4.5 with a Sonic or Supersonic Jet Exhausting Normal to the Surface," NASA TN D-1935, 1963.
7. Wallis, S., "Innovative Transverse Jet Interaction Arrangements in Supersonic Crossflow," M.S. Thesis, Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, Dec. 2001.
8. Morris, M., and Donovan, J., "Application of Pressure and Temperature Sensitive Paints to High Speed Flows," AIAA Paper 94-2231, June 1994.
9. Crites, R. C., "Pressure Sensitive Paint Technique," Von Kármán Inst. for Fluid Dynamics, Lecture Series 1993-05, Measurement Techniques, April 1993.
10. Wilcox, D. C., Turbulence Modeling for CFD, 2nd ed., DCW Industries, Inc., La Canada, CA, 1998.
11. Wilcox, D. C., "Comparison of Two-Equation Turbulence Models for Boundary Layers with Pressure Gradient," AIAA Journal, Vol. 38, No. 8, 1993, pp. 1414-1421.
12. Payne, J. L., Roy, C. J., and Beresh, S. J., "A Comparison of Turbulence Models for a Supersonic Jet in Transonic Cross Flow," AIAA Paper 2001-1048, Jan. 2001.
13. Roger, R. P., and Chan, S. C., "Parameters Affecting Penetration of a Single Jet into a Supersonic Crossflow: A CFD Study, II," AIAA Paper 98-0425, Jan. 1998.
14. Nedungadi, A., and Lewis, M. J., "A Numerical Study of Fuel Mixing Enhancement Using Oblique Shock/Vortex Interactions," AIAA Paper 96-2920, July 1996.
15. Hsieh, T., "Analysis of the Scaling Effects for Missile Configuration with Lateral Thruster," AIAA Paper 99-0810, Jan. 1999.
16. Nadungadi, A., and Lewis, M. J., "Computational Study of the Flowfields Associated with Oblique Shock Vortex Interactions," AIAA Journal, Vol. 34, No. 12, 1996, pp. 2545-2553.
17. McDaniel, J., Glass, C., Staack, D., and Miller, C., "Experimental and Computational Comparison of an Underexpanded Jet Flowfield," AIAA Paper 2002-0305, Jan. 2002.
18. GASP 3.2 User Manual, AeroSoft, Blacksburg, VA, 1997.
19. GASP 4.0 User Manual, AeroSoft, Blacksburg, VA, 2001.
20. Peery, K. M., and Imlay, S. T., "Blunt-Body Flow Simulations," AIAA Paper 88-2904, July 1988.
21. Viti, V., "Numerical Studies of the Jet Interaction Flowfield with a Main Jet and an Array of Smaller Jets," Ph.D. Dissertation, Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, Sept. 2002; also URL: http://scholar.lib.vt.edu/theses/ [cited 18 Sept. 2002].
22. GRIDGEN Version 13.3 User Manual, Pointwise, Inc., Bedford, TX, 1999.
23. Vinokur, M., "On One-Dimensional Stretching Functions for Finite Difference Calculations," Journal of Computational Physics, Vol. 50, No. 3, 1983, pp. 215-234.
24. Bardina, J. E., Huang, P. G., and Coakley, T. J., "Turbulence Modeling Validation, Testing and Development," NASA TM 110446, April 1997.
25. Roache, P. J., Verification and Validation in Computational Science and Engineering, Hermosa, Albuquerque, NM, 1998.
26. Roy, C. J., "Grid Convergence Error Analysis for Mixed-Order Numerical Schemes," AIAA Paper 2001-2006, June 2001.
27. Viti, V., Schetz, J., and Neel, R., "Numerical Studies of the Jet Interaction Flowfield with a Main Jet and an Array of Smaller Jets," International Congress of Aeronautical Sciences, ICAS Paper 2002-4.7.1, Sept. 2002.
28. Chenault, C. F., and Beran, P. S., "K-ε and Reynolds Stress Turbulence Model Comparisons for Two-Dimensional Injection Flows," AIAA Journal, Vol. 36, No. 8, 1998, pp. 1401-1412.