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Publicationspublications

Journal Articlesjournal articles

  • Broughton, B.A. and Selig, M.S., "Hybrid Inverse Design Method for Nonlifting Bodies in Incompressible Flow," Journal of Aircraft, Vol. 43 No. 6, Nov-Dec 2006, pp. 1770-1781.
  • Deters, R.W., Dimock, G.A., and Selig, M.S., "Icing Encounter Flight Simulator," Journal of Aircraft, Vol. 43, No. 5, Sept-Oct 2006, pp. 1528-1537.
  • Selig, M.S. and McGranahan, B.D., "Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines," ASME Journal of Solar Energy Engineering, Vol. 126, November 2004, pp. 986-1001.
  • Gopalarathnam, A., Broughton, B.A., McGranahan, B.D., and Selig, M.S., "Design of Low Reynolds Number Airfoils with Trips," Journal of Aircraft, Vol. 40, No. 4, 2003, pp. 768-775.
  • Gopalarathnam, A. and Selig, M.S., "Hybrid Inverse Airfoil Design Method for Complex Three-Dimensional Surfaces," Journal of Aircraft, Vol. 39, No. 3, 2002, pp. 409-417.
  • Gopalarathnam, A. and Selig, M.S., "A Design Methodology for Low-Speed Natural Laminar Flow Airfoils," Journal of Aircraft, Vol. 38, No. 1, 2001, pp. 57-63.
  • Whale, J., Fisichella, C.J., and Selig, M.S., "Correcting Inflow Measurements from Wind Turbines Using a Lifting-Surface Code," ASME Journal of Solar Energy Engineering, Vol. 122, November 2000, pp. 196-202.
  • Du, Z. and Selig, M.S., "The Effect of Rotation on the Boundary Layer of a Wind Turbine Blade," Renewable Energy, Elsevier, Vol. 20, No. 2, 2000, pp. 167-181.
  • Giguère, P., Selig, M.S., and Tangler, J.L., "Blade Design Trade-Offs Using Low-Lift Airfoils for Stall-Regulated HAWTs," ASME Journal of Solar Energy Engineering, Vol. 121, November 1999, pp. 217-223.
  • Giguère, P. and Selig, M.S., "Aerodynamic Effects of Leading-Edge Tape on Airfoils at Low Reynolds Numbers," Wind Energy Journal, Vol. 2, No. 3, July-September 1999, pp. 125-136.
  • Jasinski, W.J. and Selig, M.S, "Experimental Study of Open-Wheel Race-Car Front Wings," SAE 1998 Transactions - Journal of Passenger Cars, Vol. 107, Section 6, 1999.
  • Saeed, F., Selig, M.S., Bragg, M.B., and Addy, H. E., "Hybrid Airfoil Design Procedure Validation for Full-Scale Ice Accretion Simulation," Journal of Aircraft, Vol. 36, No. 5, September-October 1999, pp. 769-776.
  • Gopalarathnam, A. and Selig, M.S., "A Multipoint Inverse Method for Multi-Element Airfoil Design," Journal of Aircraft, Vol. 35, No. 3, May-June 1998, pp. 398-404.
  • Giguère, P. and Selig, M.S., "New Airfoils for Small Horizontal Axis Wind Turbines," ASME Journal of Solar Energy Engineering, Vol. 120, May 1998, pp. 108-114.
  • Saeed, F., Selig, M.S., and Bragg, M.B., "Hybrid Airfoil Design Method to Simulate Full-Scale Ice Accretion throughout a Given CL Range," Journal of Aircraft, Vol. 35, No. 2, March-April 1998, pp. 233-239.
  • Jasinski, W.J., Noe, S.C., Selig, M.S., and Bragg, M.B., "Wind Turbine Performance under Icing Conditions," ASME Journal of Solar Energy Engineering, Vol. 120, February 1998, pp. 60-65.
  • Giguère, P. and Selig, M.S., "Desirable Airfoil Characteristics for Large Variable-Speed Horizontal Axis Wind Turbines," ASME Journal of Solar Energy Engineering, Vol. 119, August 1997, pp. 253-260.
  • Giguère, P. and Selig, M.S., "Low Reynolds Number Airfoils for Small Horizontal Axis Wind Turbines," Wind Engineering, Vol. 21, No. 6, 1997, pp. 367-380.
  • Giguère, P. and Selig, M.S., "Freestream Velocity Measurements for Two-Dimensional Testing with Splitter Plates," AIAA Journal, Vol. 35, No. 7, July 1997, pp. 1195-1200.
  • Saeed, F., Selig, M.S., and Bragg, M.B., "A Design Procedure for Subscale Airfoils with Full-Scale Leading-Edges for Ice Accretion Testing," Journal of Aircraft, Vol. 34, No. 1, January-February 1997, pp. 94-100.
  • Selig, M.S. and Guglielmo, J.J., "High-Lift Low Reynolds Number Airfoil Design," Journal of Aircraft, Vol. 34, No. 1, January-February 1997, pp. 72-79.
  • Saeed, F. and Selig, M.S., "A Multipoint Inverse Airfoil Design Method for Slot-Suction Airfoils," Journal of Aircraft, Vol. 33, No. 4, July-August 1996, pp. 708-715.
  • Guglielmo, J.J. and Selig, M.S., "Spanwise Variations in Profile Drag for Airfoils at Low Reynolds Numbers," Journal of Aircraft, Vol. 33, No. 4, July-August 1996, pp. 699-707.
  • Selig, M.S. and Coverstone-Carroll, V.L., "Applications of a Genetic Algorithm to Wind Turbine Design," ASME Journal of Energy Resources Technology, Vol. 118, March 1996, pp. 22-28.
  • Selig, M.S. and Tangler, J.L., "Development and Application of a Multipoint Inverse Design Method for Horizontal Axis Wind Turbines," Wind Engineering, Vol. 19, No. 2, 1995, pp. 91-105.
  • Selig, M.S., Maughmer, M.D., and Somers, D.M., "A Natural-Laminar-Flow Airfoil for General-Aviation Applications," Journal of Aircraft, Vol. 32, No. 4, July-August 1995, pp. 710-715.
  • Selig, M.S., "Multipoint Inverse Design of an Infinite Cascade of Airfoils," AIAA Journal, Vol. 32, No. 4, April 1994, pp. 774-782.
  • Selig, M.S. and Maughmer, M.D., "Generalized Multipoint Inverse Airfoil Design," AIAA Journal, Vol. 30, No. 11, November 1992, pp. 2618-2625.
  • Dini, P., Selig, M.S., and Maughmer, M.D., "Simplified Linear Stability Transition Prediction Method for Separated Boundary Layers," AIAA Journal, Vol. 30, No. 8, August 1992, pp. 1953-1961.
  • Selig, M.S. and Maughmer, M.D., "Multipoint Inverse Airfoil Design Method Based on Conformal Mapping," AIAA Journal, Vol. 30, No. 5, May 1992, pp. 1162-1170.
  • Selig, M.S. and Smits, A.J., "Effect of Periodic Blowing on Attached and Separated Supersonic Turbulent Boundary Layers," AIAA Journal, Vol. 29, No. 10, October 1991, pp. 1651-1658.
  • Selig, M.S., Andreopoulos, J., Muck, K.C., Dussauge, J.P., and Smits, A.J., "Turbulence Structure in a Shock Wave/Turbulent Boundary-Layer Interaction," AIAA Journal, Vol. 27, No. 7, July 1989, pp. 862-869.

Monographsmonographs

  • Selig, M.S., "Low Reynolds Number Airfoil Design," VKI Lecture Series - Low Reynolds Number Aerodynamics on Aircraft Including Applications in Emerging UAV Technology, von Karman Institute for Fluid Dynamics (VKI) Lecture Series, RTO/AVT-VKI-104, November 2003.

Conference PapersConference Papers

  • Deters, R.W. and Selig, M.S., "Static Testing of Micro Propellers," AIAA 26th Applied Aerodynamics Conference, AIAA Paper 2008-6246, Honolulu, Hawaii, August 2008
  • Uhlig, D. and Selig, M.S., "Post Stall Propeller Behavior at Low Reynolds Numbers," AIAA 46th Aerospace Sciences Meeting, AIAA Paper 2008-407, Reno, NV, Jan 2008.
  • Clarke, J.P., Cerven, K., March, J., Olszewski, M., Wheaton, B., Williams, M., Yu, J., Selig, M.S., Loth, E. and Burton, R.L, "Supersonic Aircraft for Reusable Rocket Air-Launch (SARRA)," AIAA/ASME/SAE/ASEE 43rd Joint Propulsion Conference, AIAA Paper 2007-5841, Cincinnati, OH, July 2007.
  • Bovais, C., Levy, D., Page, G., Powell, S., Selig, M.S., and Zickur, T., "Writing the Rules: An inside Look at the AIAA Student Design/Build/Fly Competition," AIAA 6th Aviation Technology, Integration and Operations Conference (ATIO), AIAA Paper 2006-7832, Wichita, Kansas, 2006.
  • Mallipudi, S.V. and Selig, M.S. and Long, K., "Use of a Four-Hole Cobra Pressure Probe to Determine the Unsteady Wake Characteristics of Rotating Objects Paper Number," AIAA 24th Aerodynamic Measurement Technology and Ground Testing Conference, AIAA Paper 2004-2299, Portland, Oregon, June 2004.
  • Selig, M.S. and McGranahan, B.D., "Wind Tunnel Tests of Six Airfoils for Use on Small Wind Turbines," AIAA 42nd Aerospace Sciences Meeting, AIAA Paper 2004-1188, Reno, NV, January 2004.
  • Deters, R.W., Broughton, B.A., and Selig, M.S., "A Retrospective: Development of Simulation Models for the 1903 and 1905 Wright Flyers,"AIAA 42nd Aerospace Sciences Meeting, AIAA Paper 2004-0211, Reno, NV, January 2004.
  • McGranahan, B.D. and Selig, M.S., "Surface Oil Flow Measurements on Several Airfoils at Low Reynolds Numbers," AIAA 42nd Applied Aerodynamics Conference, AIAA Paper 2003-4067, Orlando, FL, June 2003.
  • Bragg, M.B., Basar, T., Perkins, W.R., Selig, M.S., Voulgaris, P.G., Melody, J.W., and Sarter, N., "Smart Icing Systems for Aircraft Icing Safety," FAA In-flight Icing / Ground De-icing International Conference, SAE Paper 2003-01-2100, Chicago, IL, June 2003.
  • Dimock, G.A. and Selig, M.S., "The Aerodynamic Benefits of Self-Organization in Bird Flocks," AIAA 41st Aerospace Sciences Meeting, AIAA Paper 2003-0608, Reno, NV, January 2003.
  • Dimock, G.A., Deters, R.W., and Selig, M.S., "Icing Scenarios with the Icing Encounter Flight Simulator," AIAA 41st Aerospace Sciences Meeting, AIAA Paper 2003-0023, Reno, NV, January 2003.
  • Gardner, B.A. and Selig, M.S., "Airfoil Design Using a Genetic Algorithm and an Inverse Method," AIAA 41st Aerospace Sciences Meeting, AIAA Paper 2003-0043, Reno, NV, January 2003.
  • Broughton, B.A. and Selig, M.S., "A Hybrid Inverse Design Method for Non-Lifting Bodies in Incompressible Flow," AIAA 41st Aerospace Sciences Meeting, AIAA Paper 2003-0213, Reno, NV, January 2003.
  • Soso, M. and Selig, M.S., "An Angle of Attack Correction Scheme for the Design of Low Aspect Ratio Wings with Endplates," SAE Motorsports Engineering Conference and Exposition, SAE Paper No 02, MSEC-15, Indianapolis, IN, November 2002.
  • Broughton, B.A., and Selig, M.S., "A Hybrid Inverse Design Method for Axisymmetric Bodies in Incompressible Flow," AIAA 20th Applied Aerodynamics Conference, AIAA Paper 2002-3142, St Louis, MO, June 2002.
  • Deters, R.W., Dimock, G.A., and Selig, M.S., "Icing Encounter Flight Simulator with an Integrated Smart Icing System," AIAA Modeling and Simulation Technologies Conference, AIAA Paper 2002-4599, Monterey, CA, August 2002.
  • Sehgal, B., Deters, R.W., and Selig, M.S., "Icing Encounter Flight Simulator," AIAA 40th Aerospace Sciences Meeting, AIAA Paper 2002-0817, Reno, NV, January 2002.
  • Bragg, M.B., Basar, T., Perkins, W.R., Sarter, N.B., Selig, M.S., Voulgaris, P.G. and Melody, J.W., "Smart Icing Systems for Aircraft Icing Safety," AIAA 40th Aerospace Sciences Meeting, AIAA Paper 2002-0813, Reno, NV, January 2002.
  • Uppuluri, S. and Selig, M.S., "Hybrid Wing Design to Match Full-Scale Wing Ice Accretion," AIAA 40th Aerospace Sciences Meeting, AIAA Paper 2002-0243, Reno, NV, January 2002.
  • Gopalarathnam, A., Broughton, B.A, McGranahan, B.D, and Selig, M.S., "Design of Low Reynolds Number Airfoils with Trips," AIAA 19th Applied Aerodynamics Conference, AIAA Paper 2001-2463, Anaheim, CA, June 2001.
  • Selig, M.S., Gopolarathnam, A., Giguère, P., and Lyon, C.A., "Systematic Airfoil Design Studies at Low Reynolds Numbers," Proceedings of the Conference on Fixed, Flapping, and Rotary Wing Vehicles at Very Low Reynolds, T.J. Mueller (ed.), Notre Dame, IN, June 2000.
  • Gopalarathnam, A. and Selig, M.S., "A Hybrid Approach to Inverse Design of Complex Aerodynamic Systems," AIAA 38th Aerospace Sciences Meeting, AIAA Paper 2000-0784, Reno, NV, January 2000.
  • Giguère, P. and Selig, M.S., "Blade Geometry Optimization for the Design of Wind Turbine Rotors," AIAA 38th Aerospace Sciences Meeting, AIAA Paper 2000-0045, Reno, NV, January 2000.
  • Gopalarathnam, A. and Selig, M.S., "A Hybrid Method for Multipoint Inverse Wing Design," AIAA 37th Aerospace Sciences Meeting, AIAA Paper 99-0401, Reno, NV, January 1999.
  • Gopalarathnam, A. and Selig, M.S., "A Design Methodology for Low-Speed Natural Laminar Flow Airfoils," AIAA 37th Aerospace Sciences Meeting, AIAA Paper 99-0399, Reno, NV, January 1999.
  • Whale, J. and Selig, M.S., "Correcting Inflow Measurements from HAWTs Using a Lifting-Surface Code," AIAA 37th Aerospace Sciences Meeting, AIAA Paper 99-0040, Reno, NV, January 1999.
  • Giguère, P. and Selig, M.S., "Blade Design Tradeoffs Using Low-Lift Airfoils for Stall-Regulated HAWTs," AIAA 37th Aerospace Sciences Meeting, AIAA Paper 99-0036, Reno, NV, January 1999. Also, NREL/CP-500-26091, Golden, CO, April 1999.
  • Jasinski, W.J. and Selig, M.S, "Experimental Study of Open-Wheel Race-Car Front Wings," SAE Motorsports Engineering Conference and Exposition, SAE Paper No 983042, Dearborn, MI, November 1998.
  • Gopalarathnam, A. and Selig, M.S., "A Multipoint Viscous Design Method for Multi-Element Airfoils," AIAA 16th Applied Aerodynamics Conference, AIAA Paper 98-2404, Albuquerque, NM, June 1998.
  • Raj, N. and Selig, M.S., "Capabilities of WTPREP for Blade Airfoil Data for HAWTs," American Wind Energy Association WINDPOWER 1998 Conference, Bakersfield, CA, April 1998.
  • Giguère, P. and Selig, M.S., "Aerodynamic Effects of Leading-Edge Tape on Airfoils at Low Reynolds Numbers," American Wind Energy Association WINDPOWER 1998 Conference, Bakersfield, CA, April 1998.
  • Du, Z. and Selig, M.S., "The Effect of Rotation of the Boundary Layer of a Wind Turbine Blade," American Wind Energy Association WINDPOWER 1998 Conference, Bakersfield, CA, April 1998.
  • Filippone, A. and Selig, M.S., "Low-Aspect-Ratio Wings for Wing-Ships," AIAA 36th Aerospace Sciences Meeting, AIAA Paper 98-0761, Reno, NV, January 1998.
  • Ninham, C.P. and Selig, M.S., "A Real-Time Atmospheric Turbulence Model for Aircraft Flight Simulators," AIAA 36th Aerospace Sciences Meeting, AIAA Paper 98-0688, Reno, NV, January 1998.
  • Saeed, F., Selig, M.S., and Bragg, M.B., "Experimental Validation of Hybrid Airfoil Design Procedure for Full-Scale Ice Accretion Simulation," AIAA 36th Aerospace Sciences Meeting, AIAA Paper 98-0199, Reno, NV, January 1998.
  • Du, Z. and Selig, M.S., "A 3-D Stall-Delay Model for Horizontal Axis Wind Turbine Performance Prediction," ASME/AIAA Joint Wind Energy Symposium, AIAA Paper 98-0021, Reno, NV, January 1998.
  • Giguère, P. and Selig, M.S., "Aerodynamic Blade Design Methods for Horizontal Axis Wind Turbines," 1997 Canadian Wind Energy Conference, Quebec City, Quebec, Canada, October 1997.
  • Gopalarathnam, A., Selig, M.S. and Hsu, F., "Design of High-Lift Airfoils for Low-Aspect Ratio Wings with Endplates," AIAA 15th Applied Aerodynamics Conference, AIAA Paper 97-2232, Atlanta, GA, June 1997.
  • Tangler, J.L. and Selig, M.S., "An Evaluation of an Empirical Model for Stall Delay Due to Rotation for HAWTs," American Wind Energy Association WINDPOWER 1997 Conference, Austin, TX, June 1997.
  • Ninham, C. and Selig, M.S., "An Interactive Windows 95/NT Version of PROPID for the Aerodynamic Design of Horizontal Axis Wind Turbines," American Wind Energy Association WINDPOWER 1997 Conference, Austin, TX, June 1997.
  • Giguère, P. and Selig, M.S., "New Airfoils for Small Horizontal-Axis Wind Turbines," American Wind Energy Association WINDPOWER 1997 Conference, Austin, TX, June 1997.
  • Jasinski, W.J, Noe, S.C., Selig, M.S., and Bragg, M.B., "Wind Turbine Performance under Icing Conditions," ASME/AIAA Joint Wind Energy Symposium, AIAA Paper 97-0977, Reno, NV, January 1997.
  • Lyon, C.A., Selig, M.S., and Broeren, A.P., "Boundary Layer Trips on Airfoils at Low Reynolds Numbers," AIAA 35th Aerospace Sciences Meeting, AIAA Paper 97-0511, Reno, NV, January 1997.
  • Saeed, F., Selig, M.S., and Bragg, M.B., "A Hybrid Airfoil Design Method to Simulate Full-Scale Ice Accretion Throughout a Given CL-Range," AIAA 35th Aerospace Sciences Meeting, AIAA Paper 97-0054, Reno, NV, January 1997.
  • Fisichella, C.J. and Selig, M.S., "A Comparison of the Inflow Predictions of Three Wind Turbine Rotor Aerodynamic Analysis Codes," American Wind Energy Association WINDPOWER 1996 Conference, Denver, CO, June 1996.
  • Giguère, P. and Selig, M.S., "Aerodynamic Performance of Small Wind Turbines Operating at Low Reynolds Numbers," American Wind Energy Association WINDPOWER 1996 Conference, Denver, CO, June 1996.
  • Giguère, P. and Selig, M.S., "Desirable Airfoil Characteristics for Large Variable-Speed Horizontal Axis Wind Turbines," American Wind Energy Association WINDPOWER 1996 Conference, Denver, CO, June 1996.
  • Gopalarathnam, A. and Selig, M.S., "A Multipoint Inverse Method for Multi-Element Airfoil Design," AIAA 14th Applied Aerodynamics Conference, AIAA Paper 96-2396, New Orleans, LA, June 1996.
  • Giguère, P. and Selig, M.S., "Freestream Velocity Measurements and Corrections for Two-Dimensional Testing with Splitter Plates," AIAA 14th Applied Aerodynamics Conference, AIAA Paper 96-2388, New Orleans, LA, June 1996.
  • Saeed, F., Selig, M.S. and Bragg, M.B., "A Design Procedure for Subscale Airfoils with Full-Scale Leading Edges for Ice Accretion Testing," AIAA 34th Aerospace Sciences Meeting, AIAA Paper 96-0635, Reno, NV, January 1996.
  • Selig, M.S., Guglielmo, J.J., Broeren, A.P. and Giguère, P., "Experiments on Airfoils at Low Reynolds Numbers," AIAA 34th Aerospace Sciences Meeting, AIAA Paper 96-0062, Reno, NV, January 1996.
  • Saeed F. and Selig, M.S., "A New Class of Airfoils with Slot-Suction," AIAA 34th Aerospace Sciences Meeting, AIAA Paper 96-0058, Reno, NV, January 1996.
  • Saeed, F. and Selig, M.S., "A Multipoint Inverse Airfoil Design Method for Slot-Suction Airfoils," AIAA 13th Applied Aerodynamics Conference, AIAA Paper 95-1857, San Diego, CA, June 1995.
  • Guglielmo, J.J., and Selig, M.S., "Large Spanwise Drag Variations in Profile Drag for Airfoils at Low Reynolds Numbers," AIAA 13th Applied Aerodynamics Conference, AIAA Paper 95-1783, San Diego, CA, June 1995.
  • Zych, T. and Selig, M.S., "Preliminary Design and Cost Analysis of a Family of Unmanned Aerial Vehicles," AIAA 13th Applied Aerodynamics Conference, AIAA Paper 95-1883, San Diego, CA, June 1995.
  • Selig, M.S. and Coverstone-Carroll, V.L., "Application of a Genetic Algorithm to Wind Turbine Design," ASME ETCE 14th Wind Energy Symposium, Houston, TX, January 1995.
  • Selig, M.S. and Guglielmo, J.J., "High-Lift Low Reynolds Number Airfoil Design," AIAA 12th Applied Aerodynamics Conference, AIAA Paper 94-1866, Colorado Springs, CO, June 1994.
  • Selig, M.S. and Tangler, J.L., "A Multipoint Inverse Design Method for Horizontal Axis Wind Turbines," American Wind Energy Association WINDPOWER 1994 Conference, Minneapolis, MN, May 1994.
  • Selig, M.S., "Multi-Point Inverse Design of an Infinite Cascade of Airfoils," AIAA 10th Applied Aerodynamics Conference, AIAA Paper 92-2650, Palo Alto, CA, June 1992.
  • Selig, M.S. and Maughmer, M.D., "Generalized Multi-Point Inverse Airfoil Design," AIAA 9th Applied Aerodynamics Conference, AIAA Paper 91-3333, Baltimore, MD, September 1991.
  • Dini, P., Selig, M.S., and Maughmer, M.D., "A Simplified en Method for Separated Boundary Layers," AIAA 9th Applied Aerodynamics Conference, AIAA Paper 91-3285, Baltimore, MD, September 1991.
  • Selig, M.S. and Maughmer, M.D., "A Multi-Point Inverse Airfoil Design Method Based on Conformal Mapping," AIAA 29th Aerospace Sciences Meeting, AIAA Paper 91-0069, Reno, NV, January 1991.
  • Selig, M.S., Giguère, P., Guglielmo, J.J., and Broeren, A.P., "Wind Tunnel Test Results of Five Free Flight Airfoils," National Free Flight Society Symposium Proceedings, Muncie, IN, June 1995.
  • Selig, M.S., Maughmer, M.D., and Somers, D.M., "An Airfoil for General Aviation Applications," DOT/FAA/CT-90/11, Proceedings of the 1990 AIAA/FAA Joint Symposium on General Aviation Systems, Ocean City, NJ, April 1990, pp. 280-291.
  • Selig, M.S., Smits, A.J., and Fernando, E.M., "Periodic Slot Blowing of a Supersonic Turbulent Boundary Layer," International Workshop on the Physics of Turbulent Compressible Mixing, Princeton, NJ, October 1988.
  • Selig, M.S., "Dynamic Control of Unsteady Shock-Wave/Turbulent Boundary-Layer Interactions," NASA Langley Research Center, AIAA 1988 Mid-Atlantic Regional Student Paper Conference, Hampton, VA, April 1988.
  • Selig, M.S., Andreopoulos, J., Muck, K.C., Dussauge, J.P., and Smits, A.J., "Simultaneous Wall-Pressure and Mass-Flux Measurements Downstream of a Shock-Wave/Turbulent Boundary-Layer Interaction," AIAA 25th Aerospace Sciences Meeting, AIAA Paper 87-0550, Reno, NV, January 1987.
  • Maughmer, M.D. and Selig, M.S., "Low Reynolds Number Airfoil Design," Proceedings of the Conference on Low Reynolds Number Airfoil Aerodynamics, T.J. Mueller (ed.), Notre Dame, IN, June 1985.
  • Selig, M.S., "The Design of Airfoils at Low Reynolds Numbers," AIAA 23rd Aerospace Sciences Meeting, AIAA Paper 85-0074, Reno, NV, January 1985.

Book ContributionsBook Contributions

  • Selig, M.S., Gopalaratham, A., Giguère, P., and Lyon, C.A., "Systematic Airfoil Design Studies at Low Reynolds Numbers," Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications, edited by T.J. Mueller, Progress in Astronautics and Aeronautics Series, AIAA, Vol. 195, 2001.
  • Selig, M.S. and Smits, A.J., "The Dynamic Behavior of a Shock-Wave/Turbulent Boundary Layer Interaction," Zoran P. Zaric Memorial International Seminar, edited by S.J. Kline and N.H. Afgan, Near-Wall Turbulence, Hemisphere Publishing Corp., New York, 1990.
  • Donovan, J.F. and Selig, M.S., "Low Reynolds Number Airfoil Design and Wind Tunnel Testing at Princeton University," Lecture Notes in Engineering, edited by T.J. Mueller, Vol. 54, Springer-Verlag, 1989, pp. 39-57.

Booksbooks

  • Selig, M.S. and McGranahan, B.D., Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines, National Renewable Energy Laboratory, NREL/SR-500-34515, Oct 2004, 133 pages. Also to appear as Summary of Low-Speed Airfoil Data, Vol 4. Six airfoils tested at Reynolds Numbers ranging from 100,000 to 500,000. [NREL report download]
  • Lyon, C.A., Broeren, A.P., Giguère, P., Gopalarathnam, A., and Selig, M.S., Summary of Low-Speed Airfoil Data, Vol. 3, SoarTech Publications, Virginia Beach, VA, 1998, 418 pages. Thirty-seven airfoils tested at Reynolds Numbers ranging from 60,000 to 500,000. [book available here]
  • Selig, M.S., Lyon, C.A., Giguère, P., Ninham, C.N., and Guglielmo, J.J., Summary of Low-Speed Airfoil Data, Vol. 2, SoarTech Publications, Virginia Beach, VA, 1996, 252 pages. Twenty-five airfoils tested at Reynolds Numbers ranging from 40,000 to 400,000.[book available here]
  • Selig, M.S., Guglielmo, J.J., Broeren, A.P., and Giguère, P., Summary of Low-Speed Airfoil Data, Vol. 1, SoarTech Publications, Virginia Beach, VA, 1995, 292 pages. Thirty-four airfoils tested at Reynolds Numbers ranging from 30,000 to 500,000. [book available here]

Technical ReportsTechnical Reports

  • Deters, R.W. and Selig, M.S., "Wind Tunnel Testing of the ICON 021816 LSA Airfoil," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-09, UILU ENG 08-0509, prepared for ICON Aircraft Inc., Los Angeles, CA, December 2008, 70 pages.
  • Deters, R.W. and Selig, M.S., "Wind Tunnel Testing of Three Airfoils for Northern Power Systems," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-08, UILU ENG 08-0508, prepared for Northern Powrer Systems, Inc., Barre, VT, December 2008, 96 pages.
  • Deters, R.W. and Selig, M.S., "Airfoil Performance Tests for the Global Observer Unmanned Aircraft System - Phase II," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-07, UILU ENG 08-0507, prepared for AeroVironment, Inc., Monrovia, CA, December 2008, 108 pages.
  • Deters, R.W. and Selig, M.S., "Airfoil Performance Tests for the Global Observer Unmanned Aircraft System - Phase I," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-06, UILU ENG 08-0506, prepared for AeroVironment, Inc., Monrovia, CA, December 2008, 105 pages.
  • Deters, R.W. and Selig, M.S., "Low Reynolds Number Airfoil Testing of a Dynamic Flap Airfoil," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-05, UILU ENG 08-0505, prepared for FlexSys, Inc., Ann Arbor, MI, December 2008, 58 pages.
  • Deters, R.W. and Selig, M.S., "Airfoil Tests for Distributed On-Blade Control for Wind Turbines," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-04, UILU ENG 08-0504, prepared for Continuum Dynamics, Inc., Ewing, NJ, November 2008, 57 pages.
  • Deters, R.W. and Selig, M.S., "Wind Tunnel Tests of the E387 Airfoil with Active Flow Control at Low Reynolds Numbers," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-02, UILU ENG 08-0502, prepared for FlexSys, Inc., Ann Arbor, MI, June 2008, 77 pages.
  • Deters, R.W. and Selig, M.S., "Aerodynamic Performance of Micro Aerial Vehicle Propellers in Static Thrust Conditions," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 08-01, UILU ENG 08-0501, prepared for Spin Master Ltd, Toronto, Ontario, Canada, June 2008, 66 pages.
  • Brandt, J.B. and Selig, M.S., "Wind Tunnel Testing of Four APC Propellers," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AE 05-01, UILU-ENG-05-0501, prepared for AeroVironment, Inc., Monrovia, CA, May 2005, 48 pages.
  • Brandt, J.B. and Selig, M.S., "Wind Tunnel Testing of the Luna Rossa F1T3, R2, and W1 Airfoils," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AAE 04-03, UILU-ENG-04-0503, prepared for Luna Rossa Srl, Milano, Italy, July 2004, 71 pages.
  • Selig, M.S. and McGranahan, "Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines," NREL/SR-500-34515, Golden, CO, October 2004, 134 pages. Also to appear as Summary of Low Speed Airfoil Data, Vol 4.
  • Broughton, B.A. and Selig, M.S., "Wind Tunnel Testing of the CDI LRA 2c Airfoil," University of Illinois at Urbana-Champaign, Dept. of Aerospace Engineering, AAE 03-04, UILU-ENG-03-0504, prepared for Continuum Dynamics, Inc., Ewing, NJ, September 2003, 29 pages.
  • Broughton, B.A., Gardner, B.A., McGranahan, B.D., and Selig, M.S., "Wind Tunnel Testing of the AeroVironment Helios Airfoil, Pod and Heat Exchanger Duct," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 02-05, UILU-ENG-02-0505, prepared for AeroVironment, Inc. Monrovia, CA, December 2002, 62 pages.
  • Gardner, B.A., Broeren, A.P., and Selig, M.S., "Wind Tunnel Tests of Four Airfoils for Sailboat Rudders," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 02-04, UILU-ENG-02-0504, prepared for Farr Yacht Design, Ltd., Annapolis, MD, June 2002, 90 pages.
  • Broughton, B.A. and Selig, M.S., "Wind Tunnel Testing of the ND-LoFoil Airfoil with and without Boundary Layer Trips," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 01-05, UILU-ENG-01-0505, February 2001, 27 pages.
  • Carroll, C.A., Broughton, B.A., and Selig, M.S., "Wind Tunnel Testing of the S8022, S8024 and S8025 Airfoils with and without Boundary Layer Trips," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 01-04, UILU-ENG-01-0504, prepared for Farr Yacht Design, Ltd, Annapolis, MD, February 2001, 64 pages.
  • Carroll, C.A., Broughton, B.A., and Selig, M.S., "Wind Tunnel Testing of the S6078 Airfoil with Simulated Solar Array Configurations," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 01-03, UILU-ENG-01-0503, prepared for AeroVironment, Inc, Monrovia, CA, February 2001, 33 pages.
  • Broughton, B.A., Carroll, C.A., and Selig, M.S., "Wind Tunnel Testing of the S1052 and S1054 Flapped Airfoils for Unmanned Flying Wing Designs," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 01-02, UILU-ENG-01-0502, prepared for the Naval Research Laboratory, Washington, DC, February 2001, 76 pages.
  • Broughton, B.A., Carroll, C.A., and Selig, M.S., "Wind Tunnel Testing of the S2012, S2014 and S2016 Airfoils for Automobile Radiator Fans," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 01-01, UILU-ENG-01-0501, prepared for Siemens Canada, London, Ontario, Canada, February 2001, 37 pages.
  • Uppuluri, S., Broeren, A., and Selig, M.S., "The Design of a Hybrid Airfoil for the NACA 23012," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 00-01, UILU-ENG-00-0501, prepared for the Federal Aviation Administration, William J. Hughes Technical Center, Atlantic City International Airport, NJ, April 2000, 22 pages.
  • Whale, J. and Selig, M.S., "LSIM: A Lifting-Surface Inflow Correction Method," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 99-12, UILU-ENG-99-0512, prepared for the National Renewable Energy Laboratory, Golden, CO, in preparation.
  • Whale, J. and Selig, M.S., "Lifting-Surface Inflow Correction Method (LSIM)," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 99-11, UILU-ENG-99-0511, prepared for the National Renewable Energy Laboratory, Golden, CO, in preparation
  • Carroll, C.A., Crosby, C.P., and Selig., M.S., "High Downforce Airfoils in Ground Effect Part 2: A Trade Study for Use in Open-Wheeled Race-Car Front-Wing Design," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 99-04, UILU-ENG-99-0504, prepared for Newman-Haas Racing, Lincolnshire, IL, April 1999, CD-ROM format.
  • Carroll, C.A., Lyon, C.A, and Selig., M.S., "High Downforce Airfoils in Ground Effect Part 1: A Trade Study for Use in Open-Wheeled Race-Car Front-Wing Design," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 99-03, UILU-ENG-99-0503, prepared for Newman-Haas Racing, Lincolnshire, IL, November 1998, approx. 120 pages.
  • Gopalarathnam, G and Selig, M.S., "Design of an Airfoil for the AeroVironment Centurion Pods," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 98-09, UILU-ENG-98-0509, prepared for AeroVironment, Monrovia, CA, November 1998, 19 pages.
  • Giguère, P. and Selig, M.S., "Design of a Tapered and Twisted Blade for the NREL Combined Experiment Rotor," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, prepared under the National Renewable Energy Laboratory Subcontract No. XAF-4-14076-03, March 1998, 22 pages. Also, NREL/SR-500-26173, Golden, CO, April 1999.
  • Whale, J., Giguère, P, and Selig, M.S., "Wind Turbines for Electric Power Generation: A Critical Analysis," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 98-08, UILU-ENG-98-0508, prepared for Caterpillar, Inc, Peoria, IL, July 1998, 14 pages.
  • Selig, M.S. and Lyon, C.A., "Pathfinder Airfoil Tests: Addendum," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 98-03, UILU-ENG-98-0503, prepared for AeroVironment, Inc., Monrovia, CA 91016, February 1998, 89 pages.
  • Selig, M.S. and Lyon, C.A., "Centurion Airfoil Tests," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 98-02, UILU-ENG-98-0502, prepared for AeroVironment, Inc., Monrovia, CA, February 1998, 226 pages.
  • Giguère, P. and Selig, M.S., "Aerodynamic Blade Design for the WindLite 8-kW Wind Turbine," University of Illinois at Urbana-Champaign, Dept. of Aeronautical and Astronautical Engineering, AAE 98-01, UILU-ENG-98-0501, prepared for WindLite Company, Inc, January 1998, 25 pages.
  • Page, G. S., Bovias, C., Selig, M., and Vargas, W., (eds.), "Compilation of the Final Reports for the AIAA Design/Build/Fly Competition," AIAA, New York, NTIS Accession Number: AD-A329 477/4/XAB, August 1997, 481 pages.

PatentsPatents

  • United States Patent 6,503,058, "Airfoil Configuration for Wind Turbine," January 7, 2003 (with Kyle K. Wetzel, assigned to GE Wind Energy)
  • United States Patent 6,382,921, "Low Reynolds Number, Low Drag, High Lift Airfoil," May 7, 2002 (with William Holmes and Frank Stauder, assigned to Siemens VDO Automotive, Inc., Mississauga, CA)
  • International Patent WO 01/83983, "Airfoil Configuration for Wind Turbine," November 8, 2001 (with Kyle K. Wetzel, assigned to GE Wind Energy)
  • European Patent 1152148, "Airfoil Profiles for Wind Turbines," July 11, 2001 (with Kyle K. Wetzel, assigned to GE Wind Energy)