A computational investigation of pulsed injection into a confined, expanding crossflow

15th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2001, Pages

  Miller, Daniel N ^a   Yaglef, Patrick J ^a   Bender, Erich E ^a   Smith, Brian R ^a   Vermeulen, Peter J ^b  

^a LOCKHEED MARTIN   (United States)

^b UNIVERSITY OF CALGARY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894490769     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. Bender, E., Miller, D., Smith, B., Yagle, P., Vermeulen, P., Walker, S., 2000, Simulation of Pulsed Injection in a Crossflow Using 3-D Unsteady CFD, AIAA No. 2000-2318.
2. Eroglu, A. and Breidenthal, R.E., 1991, Effects of Periodic Disturbances on Structure and Flame Length of a Jet in a Crossflow, AIAA, Paper No. 91-0317.
3. Federspiel, J. et al., 1995, Fluidic Control of Nozzle Flow - Some Performance Measurements, AIAA, Paper No. 95-2605.
4. Gerlinger, P. et al., 1996 Numerical Simulation of Mixing for Turbulent Slot Injection, AIAA Journal, Vol. 34, No. 1.
5. Gunter, F.L. and Fahrenholz, F.E., 1961, Final Report on a Study of Rocket Thrust Control by Gas Injection, Massachusetts Institute of Technology, Naval Supersonic Laboratory, Technical Report 448.
6. Holdeman, J.D. and Walker, R.E., 1977, Mixing of a Row of Jets with a Confined Crossflow, AIAA Journal, Vol. 15, No. 2, February, 1977.
7. Krai, L.D., Donavan, J.F., Cain, A.B., and Cary, A.W., Numerical Simulation of Synthetic Jet Actuators, AIAA 97-1824.
8. Miller, D., Yagle, P., Hamstra, J., 1999, Fluidic Throat Skewing for Thrust Vectoring in Fixed- Geometry Nozzles, AIAA No. 99-0365.
9. Miller, D.N. and Catt J.A., 1995, Conceptual Dev. of Fixed-Geometry Nozzles Using Fluidic Throat-Area Control, AIAA, Paper No. 95-2603.
10. Miller, D.N., Catt J.A., and Walker, S.H., 1997, Extending Flow Control of Fixed Nozzles Through Systematic Design: Introducing Assisted Reinjection, ASME, Paper No. FEDSM97-3680.
11. Rizzeta, D.P., Visbal, M.R. and Stanek, M.J., 1998, Numerical Investigation of Synthetic Jet Flowfields, AIAA Paper No. 98-2910.
12. Roe, P.L., 1981, Approximate Riemann Solvers, J. of Comp. Physics, Vol. 43, pp. 357-372.
13. Roe, P.L., 1981, Some Contributions to the Modeling of Discontinuous Flows, Proceedings of the SIAM/SMS Seminar.
14. Smagorinski, J., 1963, General Circulation Experiments with the Primitive Equations, Mon. Weather Rev., Vol. 91, pp. 99-164.
15. Sweby, P.K., 1984, High Resolution Schemes Using Flux Limiters for Hyperbolic Conservation Laws, SIAMJ. Numer. Anal, Vol. 21, pp. 995-1101.
16. Vakili, A., Sauerwein, S., Miller, D., 1999, Pulsed Injection Applied to Nozzle Internal Flow Control, AIAA No. 99-1002.
17. Vakili, A.D., Chang, Y.K. and Wu, J.M., 1991, Vortex Rings in Uniform Crossflow, AIAA, Paper No. 91-0522.
18. van Leer, B., 1976, MUSCL, a New Approach to Numerical Gas Dynamics, Computing in Plasma Physics and Astrophysics, Germany, April, 1976.
19. Vermeulen, P.J. et al., 1988, An Experimental Study of Mixing Behavior of an Acoustically Pulsed Air Jet with a Confined Crossflow, AIAA, No. 88-3296.
20. Vermeulen, P.J. et al., 1992, Mixing of an Acoustically Excited Air Jet With a Confined Hot Crossflow, J. of Eng. for Gas Turbines and Power, Vol. 114, No. 1, pp. 46-54.
21. Vermeulen, P.J. et al., 1992, Measurements of the Entrainment Coefficient of Acoustically Pulsed Axisymmetric Free Air Jets, J. of Eng for Gas Turbines and Power, Vol. 114, No. 4, pp. 409-415.
22. Vermeulen, P.J. et al., 1996, NOx Measurements for Combustor with Acoustically Controlled Primary Zone, ASME, Paper No. 96-GT-129.
23. Walker, S., 1997, Lessons Learned in the Development of a National Program, AIAA 97-334.
24. Wing, D.J., 1994, Static Investigation of Two Fluidic Thrust-Vectoring Concepts on a Two- Dimensional C-D Nozzle, NASA TM 4574.