A computational study of a new dual throat fluidic thrust vectoring nozzle concept

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2005, Pages

  Deere, Karen A ^a,b   Berrier, Bobby L ^a,b   Flamm, Jeffrey D ^a,b   Johnson, Stuart K ^a,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Distinguished Research Associate   (United States)

^c Advanced Aircraft Systems Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS CODES; COMPUTATIONAL INVESTIGATION; COMPUTATIONAL RESULTS; COMPUTATIONAL STUDIES; CONVERGENCE ANGLE; DESIGN CYCLE; DESIGN IMPROVEMENTS; DISCHARGE COEFFICIENTS; DIVERGENCE ANGLE; FLUIDIC THRUST VECTORING; FLUIDIC THRUST VECTORING NOZZLE; INJECTION FLOW RATE; MASS FLOW; NASA LANGLEY RESEARCH CENTER; NOZZLE DESIGNS; NOZZLE PRESSURE RATIO; PRIMARY FLOW; PULSED INJECTION; THRUST VECTORING; THRUST VECTORS; TWO-DIMENSIONAL;

COMPUTATIONAL FLUID DYNAMICS; COMPUTERIZED TOMOGRAPHY; DESIGN; FLOW RATE; NASA; PROPULSION; TEST FACILITIES;

NOZZLES;

EID: 77957838804     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (37)

1. Anderson, C. J.; Giuliano, V. J.; and Wing, David J.: Investigation of Hybrid Fluidic / Mechanical Thrust Vectoring for Fixed-Exit Exhaust Nozzles. AIAA 97-3148, July 1997.
2. Giuliano, V. J.; and Wing, David J.: Static Investigation of a Fixed-Aperture Exhaust Nozzle Employing Fluidic Injection for Multiaxis Thrust Vector Control. AIAA 97-3149, July 1997.
3. Waithe, Kenrick A.: An Experimental and Computational Investigation of Multiple Injection Ports in a ConvergentDivergent Nozzle for Fluidic Thrust Vectoring. Master of Science Thesis, May 2001.
4. Deere, K. A.: Computational Investigation of the Aerodynamic Effects on Fluidic Thrust Vectoring. AIAA 2000-3598, July 2000.
5. Wing, David J.: Static Investigation of Two Fluidic Thrust-Vectoring Concepts on a Two-Dimensional ConvergentDivergent Nozzle. NASA TM-4574, December 1994.
6. Wing, David J.; and Giuliano, V. J.: Fluidic Thrust Vectoring of an Axisymmetric Exhaust Nozzle at Static Conditions. ASME FEDSM97-3228, June 1997.
7. Deere, Karen A.; and Wing, David J.: PAB3D Simulations of a Nozzle with Fluidic Injection for Yaw-Thrust-Vector Control. AIAA 98-3254, July 1998.
8. Miller, D. N.; Yagle, P. J.; and Hamstra, J. W.: Fluidic Throat Skewing for Thrust Vectoring in Fixed Geometry Nozzles. AIAA 99-0365, January 1999.
9. Yagle, P. J.; Miller, D. N.; Ginn, K. B.; and Hamstra, J. W.: Demonstration of Fluidic Throat Skewing for Thrust Vectoring in Structurally Fixed Nozzles. 2000-GT-0013, May 8-11, 2000.
10. Deere, K. A.; Berrier, B. L.; Flamm, J. D.; and Johnson, S. K.: Computational Study of Fluidic Thrust Vectoring Using Separation Control in a Nozzle. AIAA-2003-3803, June 2003.
11. Hunter, C. A.; and Deere, K. A.: Computational Investigation of Fluidic Counterflow Thrust Vectoring. AIAA 99-2669, June 1999.
12. Flamm, J. D.: Experimental Study of a Nozzle Using Fluidic Counterflow for Thrust Vectoring. AIAA 98-3255, July 1998.
13. l3Deere, K. A.: Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley Research Center. AIAA2003-3800, June 2003.
14. l4Flamm, J. D.; Berrier, B. L.; Johnson, S. K.; and Deere, K. A.: An Experimental Study of a Dual Throat Fluidic Thrust Vectoring Nozzle Concept. AIAA-2005-3503, July 2005.
15. l5Abdol-Hamid, K S.: Tne Application of 3D Marching Scheme for the Prediction of Supersonic Free Jets. AIAA 89-2897. July 1989.
16. l6Abdol-Hamid, K. S.: Application of a Multiblock/ Multizone Code (PAB3D) for the Three-Dimensional Navier-Stokes Equations. AIAA-91-2155, June 1991.
17. Carlson, J. R.: A Nozzle Internal Performance Prediction Method. NASA TP 3221, October 1992.
18. Carlson, J. R.: Computational Prediction of Isolated Performance of an Axisymmetric Nozzle at Mach Number 0.90. NASA TM 4506, February 1994.
19. Pao, S. P., Carlson, J. R., and Abdol-Hamid, K. S.: Computational Investigation of Circular-to-Rectangular Transition Ducts. Journal of Propulsion and Power, Vol. 10, No. 1, p 95-100, Jan.-Feb. 1994.
20. Abdol-Hamid, K. S.; Lakshmanan, B.; and Carlson, J. R.: Application of Navier-Stokes Code PAB3D With k-e Turbulence Model to Attached and Separated Flows. NASA TP-3480, January 1995.
21. Abdol-Hamid, K. S., Carlson, J. R., and Pao, S. P.: Calculation of Turbulent Flows Using Mesh Sequencing and Conservative Patch Algorithm. AIAA 95-2336, July 1995.
22. Pao, S. P.; and Abdol-Hamid, K. S.: Numerical Simulation of Jet Aerodynamics Using the Three-Dimensional NavierStokes Code PAB3D. NASA TP 3596, September 1996.
23. Abdol-Hamid, K. S.; Lakshmanan, B.; and Carlson, J. R.: Application of Navier-Stokes Code PAB3D With k-e Turbulence Model to Attached and Separated Flows. NASA TP-3480, January 1995.
24. Carlson, J. R.: Applications of Algebraic Reynolds Stress Turbulence Models Part 1: Incompressible Flat Plate. Journal of Propulsion and Power, Vol. 13, No. 5, p 610-619, Sept.-Oct. 1997.
25. Abdol-Hamid, K., Pao, S., Massey, S., and Elmiligui, A.: Temperature Corrected Turbulence Model for High Temperature Jet Flow. ASME Journal of Fluids Engineering, Vol. 126, No. 5, September 2004.
26. Balakrishnan, L.; and Abdol-Hamid, K. S.: A Comparative Study of Two Codes with an Improved Two-Equation Turbulence Model For Predicting Jet Plumes. AIAA 92-2604, June 1992.
27. Girimaji, S. S.: Fully-Explicit and Self-Consistent Algebraic Reynolds Stress Model. Inst. For Computer Applications in Science and Engineering, 95-82, December 1995.
28. Abdol-Hamid, K. S.: Implementation of Algebraic Stress Models in a General 3-D Navier-Stokes Method (PAB3D). NASA CR-4702, 1995.
29. Abdol-Hamid, K. S. and Girimaji, S. S.: A Two-Stage Procedure Toward the Efficient Implementation of PANS and Other Hybrid Turbulence Models. NASA/TM-2004-213260, August 2004.
30. Massey, S. J.; and Abdol-Hamid, K. S.: Enhancement and Validation of PAB3D for Unsteady Aerodynamics. AIAA 2003-1235, January 2003.
31. Elmiligui, A., Abdol-Hamid, K., and Hunter, C.: Numerical Investigation of Flow in an Over-expanded Nozzle with Porous Surfaces. AIAA 2005-4159, July 2005.
32. van Leer, B.: Flux-Vector Splitting for the Euler Equations. ICASE Report 82-30, 1982.
33. Jones, W. P.; and Launder, B. E.: The Prediction of Laminarization With a Two-Equation Model of Turbulence. Int. Journal of Heat & Mass Transfer, vol. 15, no. 2, February 1972, pp. 301-314.
34. Vakili, A. D., Chang, Y. K., and Wu, J. M.: Vortex Rings in Uniform Crossflow. AIAA Paper 91-0552, 1991.
35. Vakili, A. D., Sauerwein, S., and Miller, D. N.: Pulsed Injection Applied to Nozzle Internal Flow Control. AIAA 99-1002,1999.
36. Eroglu, A. and Breidenthal, R. E.: Effects of Periodic Disturbances on Structure and Flame Length of a Jet in a Crossflow. AIAA Paper 91-0317, 1991.
37. Miller, D. N.; Yagle, P. J.; Bender, E. E., Smith, B. R., and Vermculen, P. J.: A computational Investigation of Pulsed Injection Into a Confined, Expanding Crossflow. AIAA 2001 -3026, June 2001.