Development and application of design strategy for design of vortex generator flow control in inlets

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 17, Issue , 2006, Pages 12598-12611

  Jirásek, Adam ^a,b,c  

^a SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^b Division of Systems Technology   (Sweden)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

INTAKE SYSTEMS; MACHINE DESIGN; OPTIMIZATION; PARAMETER ESTIMATION;

MICRO VORTEX GENERATOR FLOW CONTROL; PARAMETRIC OPTIMIZATION; VORTEX GENERATOR INSTALLATION;

FLOW CONTROL;

EID: 34250896803     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-1050     Document Type: Conference Paper

References (36)

1. Goldsmith, E. L. and Seddon, J. J., Practical Intake Aerodynamic Design, AIAA Education Series, AIAA, Reston, Virginia, 1993.
2. Dagett, D. L., Kawai, R., and Friedman, D., "Blended Wing Body Systems Studies: Boundary Layer Ingestion Inlets With Active Flow Control," NASA/CR-2003-212670, Dec. 2003.
3. Campbell, R. L., Carter, M. B., Pendegraft, O. C., Friedman, D. M., and Serrano, L., "Design and Testing of a Blended Wing Body with Boundary Layer Ingestion Nacelles at High Reynolds Numbers (Invited)," AIAA Paper 2005-459, June 2005.
4. Allan, B. G., Owens, L. R., and Berrier, B. L., "Numerical Modeling of Active Flow Control in a Boundary Layer Ingesting Offset Inlet," AIAA Paper 2004-2318, June 2004.
5. Miller, D. and Addington, G., "Invited: Aerodynamic Flowfield Control Technologies for Highly Integrated Airframe Propulsion Flowpaths," AIAA Paper 2004-2625, June 2004.
6. Hamstra, J. W., Miller, D. N., Traux, P. P., Anderson, B. H., and Wendt, B. J., "Active Inlet Flow Control Technology Demonstration," ICAS-2000-6.11.2, August-September 2000.
7. Mattingly, J., Heiser, W., and Pratt, D., Aircraft Engine Design, AIAA Education Series, American Institute of Aeronautics and Astronautics, 2nd ed., 2002.
8. Kaldschmidt, G., Syltebo, B. E., and Ting, C. T., "A 727 airplane center dvict inlet low speed performance confirmation model test for refanned JT8D engines, Phase 2," NASA-CR-134534, NASA, Nov. 1973.
9. Anderson, B. H., Huang, P. S., Paschal, W. A., and Cavatorta, E., "Study of Vortex Flow Control of Inlet Distortion," Journal of Propulsion Power, Vol. 8, No. 6, 1992, pp. 1266-1272.
10. Anderson, B. H. and Gibb, J., "Vortex Generator Installation of Steady State and Dynamic Distortion," AIAA Paper 1996-3279, June 1996.
11. Anbtawi, A. J., Blackwelder, R. F., Lissaman, P. B. S., and Liebeck, R. H., "An Experimental Investigation of Boundary Layer Ingestion in a Diffusing S-duct with and without Passive Flow Control," AIAA Paper 1999-0739, Jan. 1999.
12. Wendt, B. J. and Dudek, J. C., "Development of Vortex Generator Use for a Transitioning High-Speed Inlet," Journal of Aircraft, Vol. 35, 1998.
13. Myers, R. H. and Montgomery, D. C., Response Surface Methodology, John Willey and sons, New York, 3rd ed., 1995.
14. Schmidt, R. and Laundsby, T., Understanding Design of Experiment, Academy Associates, 1995.
15. Giunta, A. A., Wojtkievicz, S. F., and Eldred, M. S., "Overview of Modern Design of Experiments Methods for Computational Simulations," AIAA Paper 2003-649, Jan. 2003.
16. Mohler, S. R., "Wind-US Flow Caluclations for the M2129 S-duct Using Structured and Unstructured Grids," NASA/CR-2003-212736, NASA, April 2003.
17. Tai, T. C., "Effect of Midwing Vortex Generators on V-22 Aircraft Forward-Flight Aerodynamics," Journal of Aircraft, Vol. 40, No. 4, 2003, pp. 623-630.
18. Anderson, B. H., Yagle, P. J., Miller, D. N., and Traux, P. P., "A Stvidy of MEMS Flow Control for the Management of Engine Distortion in Compact Inlet Systems," FEDSM99-6920, July 1999.
19. Anderson, B. H. and Keller, D. J., "A Parameter Design Methodologies for Micro-Scale Secondary Flow Control in Compact Inlets," AIAA Paper 2002-0541, June 2002.
20. Anderson, B. H. and Keller, D. J., "A Robust Design Methodology for Optimal Microscale Secondary Flow Control in Compact Inlet Diffuers," NASA TM 2002-211467, June 2002.
21. Kunik, W. G., "Application of a Computational Model for Vortex Generators in Subsonic Internal Flows," AIAA Paper 86-1458, June 1986.
22. Bender, E. E., Anderson, B. H., and Yagle, P. J., "Vortex Generator Modelling for Navier-Stokes Codes," FEDSM 99-6919, July 1999.
23. Chima, R. V., "Computational Modeling of Vortex Generators for Turbomachimery," NASA/TM-2002-211551, NASA, April 2002.
24. Dudek, J. C., "An Empirical Model for Vane-Type Vortex Generators in a Navier-Stokes Code," AIAA Paper 2005-1003, 43rd AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, Jan. 2005.
25. Jirásek, A., "Vortex-Generator Model and its Application to Flow Control," Journal of Aircraft, Vol. 42, No. 6, November-December 2005, pp. 1486-1491.
26. Montgomery, D. C., Response Surface Method, John Willey and sons., New York, 5th ed., 1995.
27. Box, G. E. P. and Mayer, R. D., "An Analysis of Unreplicated Fractional Factorials," Technometrics, 1986.
28. Daniel, C., "Use of Half-Normal Plots in Interpreting Factorial Two Level Experiment," Technometrics, 1959,
29. Giunta, A. A., "Aircraft Multidisciplinary Design Optimization Using Design of Experiments Theory and Response Surface Modeling Methods." Doctorate thesis, Virginia Polytechnic Institute, May 1997.
30. Simspon, T. W., Korte, J. J., Maurey, T. M., and Mistree, F., "Comparison of Response Surface and Kriging Models for Multidisciplinary Design Optimization," AIAA Paper 1998-4755, Jan. 1998.
31. Advisory Group for Aerospace Research & Development, "Air Intakes for High Speed Vehicles," AGARD Advisory Report 270, Fluid Dynamics Panel Working Group 13, AGARD-AR-270, 1991.
32. Seddon, J. J. and Goldsmith, E. L., Intake aerodynamics, AIAA, 3rd ed., 1995.
33. Eliasson, P., "EDGE, a Navier-Stokes solver for unstructured grids," Proc. to finite Volumes for Complex Applications III, ISBN 1 9039 9634 1, 2002. pp. 527-534.
34. Montgomery, D. C., Peck, E. A., and Vining, G. G., Introduction to Linear Regression Analysis, John Willey and sons, New York, 3rd ed., 2001.
35. Johansson, M., "FoT25 2003-2005 Propulsion Integration, Final Report," FOI-R-1572-SE, Dec. 2005.
36. Jirasek, A., "Mass Flow Boundary Conditions for Subsonic Inflow and Outflow Boundary," AIAA Paper 2005-4963, 23rd AIAA Applied Aerodynamics Conference and Exhibit, Toronto, Ontario, Canada, June 2005.