Vectoring thrust in multiaxes using confined shear layers

Journal of Fluids Engineering, Transactions of the ASME

Volumn 122, Issue 1, 2000, Pages 3-13

  Alvi, F S ^a   Strykowski, P J ^b   Krothapalli, A ^a   Forliti, D J ^b  

^a FLORIDA A AND M UNIVERSITY   (United States)

^b UNIVERSITY OF MINNESOTA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0009780498     PISSN: 00982202     EISSN: 1528901X     Source Type: Journal    
DOI: 10.1115/1.483220     Document Type: Article

References (31)

1. Herrick, P. W., 1988, “Air Combat Payoffs of Vectoring/Reversing Exhaust Nozzles” AIAA/ASME/SA E/A SEE 24th Joint Propulsion Conference, Boston, MA, Paper AIAA-88-3239.
2. Nguyen, L. T., and Gilbert, W. P., 1990, “Impact of Emerging Technologies on Future Combat Aircraft Agility,” AIAA/SFTE/DGLR/SETP Fifth Biannual Flight Test Conference, Ontario. CA, Paper AIAA 90-1304.
3. Henderson, W. P., 1990, “Propulsion System Integration in High Performance Aircraft,” Aerospace Engineering, 10, No. 2, pp. 21-25.
4. Mishler, R., and Wilkinson, T., 1992, “Emerging Airframe/Propulsion Integration Technologies at General Electric,” AIAA/SAE/ASME/ASEE 28 Joint Propulsion Conference and Exhibit, Nashville, TN. Paper AIAA 92-3335.
5. Chambers, J. R., 1992, “High-Alpha Flight Dynamics: Lessons Learned,” NASA High Angle-of-Attack Projects and Technology Conference.
6. Doonan, J. G., and Kuchar, A. P., 1992, “Scale Model Test Results of a Multi-Slotted Vectoring 2DCD Ejector Nozzle,” AIAA/SAE/ASME/ASEE 28 Joint Propulsion Conference and Exhibit, Nashville, TN, Paper AIAA 92- 3264.
7. Capone, F., Smereczniak, P., Spetnagel, D., and Thayer, E., 1992, “Comparative Investigation of Multiplane Thrust Vectoring Nozzles”, AIAA/SAE/ASME/AS EE 28 Joint Propulsion Conference and Exhibit, Nashville, TN, Paper AIAA 92-3263.
8. Snow, B. H., 1990, “Thrust Vectoring Control Concepts and Issues,” SAE Technical Paper Series,901848, Oct.
9. Asbury, S. C., and Capone, F. J., 1995, “Multiaxis Thrust-Vectoring Characteristics of a Model Representative of the F-18 High-Alpha Research Vehicle at Angles of Attack from 0 to 70 deg.” Dec., NASA Technical Paper 3531.
10. Wing, D. J., 1994, “Static Investigation of Two Fluidic Tlirust-Vectoring Concepts on a Two-Dimensional Convergent Divergent Nozzle,” NASA TM-4574.
11. Warren, R. W., 1962, “Some Parameters Affecting the Design of Bistable Fluid Amplifiers,” ASME Symposium of Fluid Jet Control Devices, Nov., pp. 75-82.
12. Comparin, R. A., Mitchell, A. E., Mueller, H. R., and Glaettli, H. M., 1962, “On the Limitations and Special Effects m Fluid Jet Amplifiers,” ASME Symposium of Fluid Jet Control Devices, pp. 65-74.
13. Gilbert, B., 1991, “Directional Control of Large Mass Flows by Fluidics,” FLUCOME’91 ASME 3rd Triennial International Symposium of Fluid Control, Measurement and Visualization.
14. Carrol, G. R., and Cox, H., 1983, “A Missile Flight Control System using Boundary Layer Thrust Vector Control,” June. Paper AIAA 83-1149.
15. Fitzgerald, R. E., and Karnpe, R. F., 1983, “Boundary Layer TVC for Missile Applications” AIAA Paper 83-1153.
16. Porzio, A. J., and Franke, M. E., 1989. “Experimental Study of a Confined Jet Thrust Vector Control Nozzle,” J. Propul. Power. 5, No. 5, pp. 596-601.
17. Grmstein, F. F., 1998, “Entrainment and Thrust Vector Control with Counter- current Rectangular Jets,” 11th ONR Propulsion Meeting. West Palm Beach, FL, pp. 34-41.
18. Hunter, C. A., and Deere, K. A., 1999, “Computational Investigation of Fluidic Counterflow Thrust Vectoring,” 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Los Angeles, CA, Paper AIAA 99-2669.
19. Strykowski, P. J., Krothapalli, A., and Forliti, D. J., 1996, “Counterflow Thrust Vectoring of Supersonic Jets,” AIAA J., 34, No. 11, pp. 2306-2314.
20. Van der Veer, M. R., and Strykowski, P. J., 1997, “Counterflow Thrust Vector Control of Subsonic Jets: Continuous and Bistable Regimes.” J. Propul. Power, 13. No. 3, pp. 412-420.
21. Young, T., 1957, “Outlines of Experiments and Inquiries Respecting Sound and Light.” Lecture to the Royal Society, also Journal of the Royal Aeronautical Society, 61. 157.
22. Strykowski, P. J., and Wilcoxon, R. K., 1993, “Mixing Enhancement due to Global Oscillations in Jets with Annular Counterflow,” AIAA J., 31, No. 3, pp. 564-570.
23. Strykowski, P. J., Krothapalli, A., and Jendoubi, S., 1996, “Hie Effect of Counterflow on the Development of Compressible Shear Layers,” J. Fluid Mech., 308, pp. 63-96.
24. Ramaswamy, M. A., Alvi, F. S., and Krothapalli, A., 1997, “Special 6-Component Jet Rig Balance for Studying New Thrust Vectoring Concepts,” 17th ICIASF Conference, Pacific Grove, CA.
25. Wishart, D. P., and Krothapalli, A., 1994, “On the Structure of a Heated Supersonic Jet,” AIAA Paper 94-0666.
26. Forliti, D. J., 1995, “Measurement of a Rectangular Mach 2 Jet Under Free and Counterflow Thrust Vectored Conditions,” M.S. thesis. Department of Mechanical Engineering, Florida State University, Tallahassee, FL.
27. Gillgrist, R. D., 1999, “A Fundamental Study of Thrust Vector Control Using Counterflow,” M.S. thesis. Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN.
28. Flamrn, J. D., 1998, “Experimental Study of a Nozzle Using Fluidic Counterflow for Thrust Vectoring,” 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & ExhibitCleveland, OH. Paper AIAA 98-3255.
29. Raman, G., Hailye, M., and Rice, E. J., 1993, “Flip-Flop Jet Nozzle Extended to Supersonic Flows,” AIAA J., 31, No. 6, pp. 1028-1035.
30. Schmid, G. F., 1996, “Design and Optimization of a Counterflowing Thrust Vectoring System, M.S. thesis, University of Minnesota. MN.
31. Strykowski, P. J., Schmid, G. F., Alvi, F. S., and Krothapalli, A., 1997, “Vectoring Thrust Using Confined Countercurrent Shear Layers.” AIAA 4th AIAA Shear Flow Control Conference, Snowmass. CO, Paper AIAA 97-1997.