In-flight receptivity experiments on a 30-degree swept-wing using micron-sized Discrete Roughness Elements

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Carpenter, Andrew L ^a   Saric, William S ^a   Reed, Helen L ^a  

^a Department of Electrical and Computer Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CROSS-FLOW INSTABILITIES; DISTURBANCE AMPLITUDE VARIATIONS; LEADING EDGE; MULTI-ELEMENT; ROUGHNESS ELEMENTS; ROUGHNESS HEIGHT; WALL SHEAR STRESS;

AEROSPACE ENGINEERING; LAMINAR FLOW; REYNOLDS NUMBER;

SWEPT WINGS;

EID: 78549241606     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (33)

1. Green, J.E., "Laminar Flow Control - Back to the Future?" AIAA 2008-3738, 2008.
2. Saric, W.S., Carrillo, R.B., Reibert, M.S., "Leading-Edge Roughness as a Transition Control Mechanism," AIAA 98-0781, 1998.
3. Saric, W.S., Reed, H.L., Banks, D.W. "Flight Testing of Laminar Flow Control in High-Speed Boundary Layers," NATO-RTOMP-AVT-111/RSM, 2005.
4. Reed, H.L., Saric, W.S., "Transition Mechanisms for Transport Aircraft," AIAA 2008-3743, 2008.
5. Saric, W.S., Reed, H.L., White, E.B., "Stability and Transition of Three-Dimensional Boundary Layers," Ann. Rev. Fluid Mech., 2003.35:413-40.
6. Reibert, M.S., Saric, W.S., Carrillo, R.B., Chapman, K.L., "Experiments in Nonlinear Saturation of Stationary Crossflow Vortices in a Swept-Wing Boundary Layer," AIAA 96-0184, 1996.
7. Wassermann P, Kloker M. "Mechanisms and control of crossflow-vortex induced transition in a three-dimensional boundary layer," J. Fluid Mech. 456:49-84, 2002.
8. White, E.B., Saric, W.S. "Secondary Instabilities of Crossflow Vortices," J. Fluid Mech. Vol. 525:275-308, 2005.
9. Morkovin, M.V., "On the many faces of transition," Viscous Drag Reduction, ed: CS Wells, pages 1-31, New York: Plenum, 1969.
10. Choudhari, M., Streett, C., "Boundary Layer Receptivity Phenomena in Three-Dimensional and High-Speed Boundary Layers," AIAA 90-5258, 1990.
11. Rhodes, R.G., Carpenter, A.L., Reed, H.L., Saric, W.S., "CFD Analysis of Flight-Test Configuration for LFC on Swept-Wings," AIAA 2008-7336, 2008.
12. Martin, M.L., Carpenter, A.L., Saric, W.S., "Swept-Wing Laminar Flow Control Studies Using Cessna O-2A Test Aircraft," AIAA 2008-1636, 2008.
13. McKnight, CW 2006. Design and Safety Analysis of an In-Flight, Test Airfoil. Master's Thesis, ETD-TAMU-2006B-AEROMcKnight.
14. Saric, WS, Carpenter, A.L, Hunt LE, McKnight CW, Schouten SM 2006b. "SWIFT - Safety Analysis for Swept-Wing Experiments." TAMUS-AE-TR-06-002, Technical Report, January 2006.
15. Saric, W.S., Carpenter, A.L., Reed, H.L., "Laminar Flow Control Flight Tests for Swept Wings: Strategies for LFC," AIAA 2008-3834, 2008.
16. Banks, D.W., van Dam, C.P., Shiu, H.J., Miller, G.M., "Visualization of In-Flight Flow Phenomena Using Infrared Thermography," NASA/TM-2000-209027, 2000.
17. Brandon, J.M., Manuel, G.S., Wright, R.E., Holmes, B.J., "In-flight flow visualization using infrared imaging," Journal of Aircraft 27:612-618, 1990.
18. Miley, S.J., van Dam, C.P., Yip L.P., Willard, P.E., Crowder, J.P., Wazlavick, R.L., "Slat transition characteristics on the NASA B737-100 aircraft using infrared imaging and hotfilm anemometry," Crowder JP (ed) Flow visualization VII. Begell House, New York, pages 950-956, 1997.
19. Schlichting, H., Gersten, K., "Boundary Layer Theory," Springer-Verlag, 2000.
20. Saric, W.S., Reed, H.L., "Crossflow Instabilities - Theory & Technology," AIAA-2003-0771, 2003.
21. White, E.B., Saric, W.S., "Application of Variable Leading-Edge Roughness for Transition Control on Swept-Wings," AIAA 2000-0283, 2000.
22. Radeztzky, R.H., Reibert, M.S., Saric, W.S., Takagi, S., "Effect of Micron-Sized Roughness on Transition in Swept-Wing Flows," AIAA 93-0076, 1993.
23. Moes, T.R., Sarma, G.R., Mangalam, S.M., "Flight Demonstration of a Shock Location Sensor Using Constant Voltage Hotfilm Anemometry," NASA TM 4806, Aug. 1997.
24. Mangalam, S.M., Maddalon, D.V., Saric, W.S., Agarwal, N.K., "Measurement of Crossflow Vortices, Attachment-Line Flow, and Transition Using Microthin Hotfilms, AIAA 90-1636, 1990.
25. Agarwal, N.K., Maddalon, D.V., Mangalam, S.M., Collier, F.S., "Crossflow Vortex and Transition Measurements by Use of Multi-element Hotfilms," AIAA J., Vol. 30, No. 9, September 1992.
26. Chapman, K.L., Glauser, M., Dagenhart, J.R., and Saric, W.S. "Application of Multipoint Correlation Techniques to Aerodynamic Flows," AIAA Paper No. 94-2279.
27. Saric, W.S. "Boundary-Layer Stability and Transition." Springer Handbook of Experimental Fluid Mechanics Springer-Verlag Berlin Heidelberg, Ed: Cameron Tropea, Alexander Yarin, John F. Foss. Chapter C.12, Section 12.3 pp. 886-896, 2007.
28. Preston, J.H., "The Determination of Turbulent Skin Friction by Means of Pitot Tubes," J. Roy. Aero. Soc. 58, 1954.
29. Patel, V.C., "Calibration of the Preston Tube and Limitations on Its Use in Pressure Gradients," J. Fluid Mech. 35(1), 1965.
30. Bechert, D.W., "Calibration of Preston Tubes," AIAA J., Vol. 34, No. 1, Pg 205 - 206.
31. Radeztsky, R.H., Reibert, M.S., Takagi, S., "A Software Solution to Temperature-Induced Hotwire Voltage Drift," Proceedings of the Third International Symposium on Thermal Anemometry, 1993.
32. Sarma, G.R., Moes, T.R., "Demonstration of skin friction measurements featuring in situ estimation of conduction loss using constant voltage anemometers and surface hotfilms," Rev. Sci. Instruments 76, 2005.
33. Bellhouse, B.J., Schultz, D.L., "Determination of mean and dynamic skin friction, separation and transition in low-speed flow with a thin-film heated element," J.Fluid Mech., Vol 24, part 2, pages 379 - 400, 1966.