Mesoflap and bleed flow control for a mach 2 inlet

AIAA Paper

Volumn , Issue , 2004, Pages 9586-9609

  Loth, E ^a   Jaiman, R ^a   Dutton, C ^a   White, S ^a   Roos, F ^b   Mace, J ^b   Davis, D ^c  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b BOEING COMPANY   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLEED SYSTEM; MASS FLOW; MESOFLAP FLOW CONTROL; SHOCK PRESSURE;

AERODYNAMICS; AIRFOILS; BOUNDARY LAYERS; COMPUTER SIMULATION; CONTROL SYSTEMS; DIFFUSERS (FLUID); FLOW CONTROL; INTAKE SYSTEMS; OPTIMIZATION; PARAMETER ESTIMATION; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; ROBUSTNESS (CONTROL SYSTEMS); SHOCK WAVES; WIND TUNNELS;

SPACE RESEARCH;

EID: 2942722645     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. Nicolai, L.M. (1975) Fundamentals of Aircraft Design METS Inc. San Jose, CA.
2. Benson, J.L. & Miller,.L.D, (1991) "Mach 5 Turbo-Ramjet Inlet Design and Performance" ISABE 91-7079, ISABE Conference, Nottingham, U.K., September, Vol. 12, pp. 746-753.
3. Carter, T.D. & Spong, E.D. (1977)"High-Speed Inlet Investigation; Vol I. Description of Program and Results" Technical Report AFFDL-TR-77-105, November, Air Force Flight Dynamics Laboratory, Wright-Patterson AFB.
4. Koenig, R.W. (1967) "Inlet Sensitivity for a Supersonic Transport" NASA TN D-3881, NASA Lewis Research Center, Cleveland, OH.
5. th AIAA/SAE/ASME/ASEE Joint Propulsion Conference, AIAA 90-2151, Orlando, FL, July.
6. E. Loth "Smart Mesoflaps for Control of Shock Boundary-Layer Interactions," AIAA Fluid Dynamics 2000, AIAA-200-2476, Denver, CO, June.
7. Raghunathan, S., (1988) "Passive Control of Shock Boundary Layer Interaction," Progress in Aerospace Science, 5, pp. 271-296.
8. Bur, R., Corbel, B., and Delery, J., (1998) "Study of Passive Control in a Transonic Shock-Wave/Boundary Layer Interaction," AIAA-2000-2476.
9. D. Gefroh, E. Loth, J.C. Dutton, and E. Hafenrichter "Aeroelastically-Deflecting Flaps in a Shock/Boundary Layer Interaction.". Journal of Fluids and Structures Vol., 17, No. 7, June 2003, Pages 1001-1016.
10. Y. Lee, E. Hafenricheter, R. Jaiman, M. Orphandies, J.C. Dutton, and E. Loth (2001) "Skin Friction Measurements in Normal Shock-Wave Boundary-Layer Interaction Control with Aeroelastic Mesoflaps", AIAA Aerospace Sciences Meeting AIAA 2002-0979. Reno NV, January (also to appear in AIAA Journal).
11. Y. Lee, E. Hafenricheter, R. Jaiman, M. Orphandies, J.C. Dutton, and E. Loth (2001) "Skin Friction Measurements in Normal Shock-Wave Boundary-Layer Interaction Control with Aeroelastic Mesoflaps", AIAA Aerospace Sciences Meeting AIAA 2002-0979. Reno NV, January (also to appear in AIAA Journal).
12. E. Hafenrichter, Y. Lee, J.C. Dutton, and E. Loth "Normal Shock Boundary-Layer Interaction Control using Aeroelastic Mesoflaps," AIAA Journal of Propulsion and Power Vol. 19, No. 3, pp. 464-472, May-June 2002.
13. R. Jaiman, E. Loth, and J.C. Dutton (2003) "Numerical Simulations of Normal Shock-Wave Boundary Layer Interaction Control using Mesoflaps," AIAA Aerospace Sciences Meeting, Reno NV, January (also to appear in AIAA Journal of Propulsion and Power).
14. R. Jaiman, E. Loth, and J.C. Dutton (2003) "Numerical Simulations of Normal Shock-Wave Boundary Layer Interaction Control using Mesoflaps," AIAA Aerospace Sciences Meeting, Reno NV, January (also to appear in AIAA Journal of Propulsion and Power).
15. R. Jaiman (2002) "Normal Shock-Wave Boundary Layer Interaction Control using Mesoflaps", M.S. Thesis, Dept. of Aeronautical & Astronautical Engineering, University of Illinois at Urbana-Champaign, October.
16. Micol, J.R. (2001) "Langley Research Center's Unitary Plan Wind Tunnel: Testing Capabilities and Recent Modernization Activities," AIAA 20 01-0456, January.
17. G.M. McLafferty and E. Ranard (1958) "Pressure Losses and Flow Coefficients of Slanted Perforations Discharging from Within a Simulated Supersonic Inlet," United Aircraft Corporation Report R-0920-1, December.
18. Erickson, G.E. (2000) "Overview of Selected Measurement Techniques for Aerodynamics Testing in the NASA Langley Unitary Plan Wind Tunnel," AIAA-2000-2396, June.