Computational investigation of the aerodynamic effects on fluidic thrust vectoring

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Deere, Karen A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; PROPULSION; REYNOLDS NUMBER;

COMPUTATIONAL FLUID DYNAMICS CODES; COMPUTATIONAL INVESTIGATION; DISCHARGE COEFFICIENTS; FLUIDIC THRUST VECTORING; FREESTREAM CONDITIONS; NOZZLE PRESSURE RATIO; REYNOLDS STRESS MODELS; THREE DIMENSIONAL SIMULATIONS;

AERODYNAMICS;

EID: 0003305022     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (35)

1. Hiley, P. E.; Wallace, H. W.; and Booz, D. E.: Nonaxisymmetric Nozzles Installed in Advanced Fighter Aircraft. J. Aircraft, Vol. 13, No. 12, December 1976, pp. 1000-1006.
2. Willard, C. M.; Capone, F. J.; Konarski, M.; and Stevens, H.L.: Static Performance of Vectoring/Reversing Nonaxisymmetric Nozzles. AIAA 840, 1977.
3. Bergman, D.; Mace, J. L.; and Tayer, E. B.: Nonaxisymmetric Nozzle Concepts for an F-lll Test Bed. AIAA 841, 1977.
4. Stevens, H. L.: F-15/Nonaxisymmetric Nozzle System Integration Study Support Program. NASA CR-135252, 1978.
5. Maiden, D. L., and Petit, I.E.: Investigation of Two-Dimensional Wedge Exhaust Nozzles for Advanced Aircraft. AIAA 1317, 1975.
6. Capone, F. J.; and Maiden, D. L.: Performance of Twin Two-Dimensional Wedge Exhaust Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2. 2. NASA TN D-8449, 1977.
7. Pendergraft, O. C. Jr.: Comparison of Axisymmetric and Nonaxisymmetric Nozzles Installed on the F-15 Configuration. AIAA 842, 1977.
8. Lander, J. A.; Nash, D. O., and Palcza, J. L.: Augmented Deflector Exhaust Nozzle/ ADEN/ Design for Future Fighters. AIAA 1318, 1975.
9. Goetz, G. F.; Young, J. H., and Palcza, J. L.: A Two-Dimensional Airframe Integrated Nozzle Design with Inflight Thrust Vectoring and Reversing Capabilities for Advanced Fighter Aircraft. AIAA 626, 1976.
10. Wasson, H. R.; and Hall, G. R.: Results of a Feasibility Study to Add Canards and ADEN Nozzle to the YF-17. AIAA 1227, 1977.
11. Berrier, B. L.; and Re, R. J.: A Review of Thrust-Vectoring Schemes for Fighter Aircraft. AIAA 78-1023, July 1978.
12. Herbst, W. B.: Supermaneuverability. Workshop on Unsteady Separated Flow, Michael S. Francis and Marvin W. Luttges, eds, AFOSR-TR-84- 3109, U.S. Air Force, May 1984, pp. 1-9.
13. Gallaway, C. R.; and Osborn, R. F.: Aerodynamics Perspective of Supermaneuverability. AIAA 85-4068, October 1985.
14. Capone, F. J.; and Mason, M. L.: Multiaxis Aircraft Control Power from Thrust Vectoring at High Angles of Attack. NASA TM-87741, June 1986.
15. Berrier, B. L.; and Mason, M. L.: Static Investigation of Post-Exit Vanes for Multiaxis Thrust Vectoring. AIAA 87-1834, June-July 1987.
16. Capone, F. J.; and Bare, E. A.: Multiaxis Control Power from Thrust Vectoring for a Supersonic Fighter Aircraft Model at Mach 0.2 to 2. 47. NASATP-2712, July 1987.
17. Taylor, J. G.: A Static Investigation of a Simultaneous Pitch and Yaw Thrust Vectoring 2-D C-D Nozzle. AIAA 88-2998, July 1988.
18. Berrier, B. L.; and Mason, M. L.: Static Performance of an Axisymmetric Nozzle with Post-Exit Vanes for Multiaxis Thrust Vectoring. NASA TP-2800, May 1988.
19. Berrier, B. L.: Results from NASA Langley Experimental Studies of Multiaxis Thrust Vectoring Nozzles. SAE TP-881481, October 1988.
20. Chiarelli, C.; Johnsen, R. K.; and Shieh, C. F.: Fluidic Scale Model Multi-Plane Thrust Vector Control Test Results. AIAA 93-2433, June 1993.
21. Giuliano, V. J.; Flugstad T. H.; Semmes, R.; and Wing, D. J.: Static Investigation and Computational Fluid Dynamics (CFD) Analysis of Flowpath Cross-Section and Trailing-Edge Shape Variations In Two Multiaxis Thrust Vectoring Nozzle Concepts. AIAA 94-3367, June 1994.
22. Federspiel, J.; Bangert, L.; Wing, D.; and Hawkes, T.: Fluidic Control of Nozzle Flow - Some Performance Measurements. AIAA 95-2605, July 1995.
23. Anderson, C. J.; Giuliano, V. J.; and Wing, D. J.: Investigation of Hybrid Fluidic/Mechanical Thrust Vectoring for Fixed-Exit Exhaust Nozzles. AIAA 97-3148, July 1997.
24. Deere, K. A.: PAB Simulations of a Nozzle with Fluidic Injection for Yaw Thrust-Vector Control. AIAA 98-3254, July 1998.
25. Hunter, C. A.; and Deere, K. A.: Computational Investigation of Fluidic Counter/low Thrust Vectoring. AIAA 99-2669, June 1999.
26. Flamm, J. D.: Experimental Study of a Nozzle Using Fluidic Counter/low for Thrust Vectoring. AIAA 98-3255, July 1998.
27. Pack, L. G.; and Seifert, A.: Periodic Excitation for Jet Vectoring and Enhanced Spreading. AIAA 99-0672, January 1999.
28. Abdol-Hamid, Khaled, S.: Implementation of Algebraic Stress Models in a General 3-D Navier- Stokes Method (PAB). NASA CR-4702, 1995.
29. Abdol-Hamid, Khaled, S.: Application of a Multiblock/Multizone Code (PAB) for the Three- Dimensional Navier-Stokes Equations. AIAA-91-2155, June 1991.
30. van Leer, B.: Flux-Vector Splitting for the Euler Equations. ICASE Report 82-30, 1982.
31. Roe, P. L.: Characteristics Based Schemes for the Euler Equations. A Numerical Review of Fluid Mechanics, 1986, pp. 337-365.
32. Abdol-Hamid, Khaled S.; Lakshmanan, B.; and Carlson, John R.: Application of Navier-Stokes Code PAB With k-£ Turbulence Model to Attached and Separated Flows. NASA TP-3480, January 1995.
33. Jones, W. P.; and Launder, B. E.: The Prediction of Lamina rization With a Two-Equation Model of Turbulence. Int. Journal of Heat & Mass Transfer, vol. 15, no. 2, February 1972, pp. 301-314.
34. Carlson, John R.: A Nozzle Internal Performance Prediction Method. NASA TP-3221, October 1992.
35. Ames Research Staff: Equations, Tables, and Charts for Compressible Flow. NACA Report 1135, 1953.