fbpx
Wikipedia

Mark D. Maughmer

Mark D. Maughmer (born January 18, 1950) is a professor of Aerospace Engineering in the Department of Aerospace Engineering at The Pennsylvania State University. He is a widely published author known throughout the world as one of the leading aerodynamicists, especially in the areas of airfoil and winglet design and analysis, wing optimization, natural laminar flow aerodynamics, and subsonic, low turbulence wind-tunnel design and operation.[1]

Mark D. Maughmer
Alma materUniversity of Illinois, 1983
Known forAerodynamics, Winglet Design
Scientific career
InstitutionsPennsylvania State University

Winglets Edit

 
PSU 90-125 winglet airfoil profile

In 1987, Peter Masak called on Maughmer about designing winglets for his sailplane to improve performance. Others had attempted to apply Richard T. Whitcomb's NASA winglets to gliders, and though they did improve climb performance, this did not offset the parasite drag penalty in high speed cruise. Masak was convinced it was possible to overcome this hurdle, and Maughmer was willing to join his quest.

By trial and error, they ultimately developed successful winglet designs for gliding competitions, and at the 1991 World Gliding Championships in Uvalde, Texas, the trophy for the highest speed went to a winglet equipped 15-meter class limited wingspan glider, exceeding the highest speed in the unlimited span Open Class, an exceptional result.[2]

The winglets were originally retrofit to production sailplanes, but now most high-performance gliders are equipped from the factory with winglets, or some other wingtip device.[3] Maughmer has consulted with German sailplane designers on winglets, non-planar wing tips, and other aerodynamic improvements incorporated in several production sailplanes.[citation needed]

Education and academics Edit

He received his Ph.D. (Aeronautical and Astronautical Engineering) from the University of Illinois in 1983, M.S. from Princeton University in 1975 and B.S. from the University of Illinois in 1972. Maughmer received the PSES Outstanding Teaching Award in 1993, the PSES Premier Teaching Award in 2001, and the Alumni Faculty Teaching Fellow Award in 2012. In 2009, Maughmer received the ASEE Fred Merryfield Design Award, a national award for teaching excellence in engineering design. He is active in the AIAA and has served on the Aircraft Design Technical Committee (1987–90). He received the AIAA/ASEE John Leland Atwood Award in 2013, and the AIAA William T. Piper Award in 2014. For the Soaring Society of America, he is chair of configuration and design for the Technical Board, serves on the board of directors for the Collegiate Soaring Association, and received the society's Exceptional Service Award in 1991. He has served on the Board of the International Organization for the Science and Technology of Soaring (OSTIV), and is currently the vice-president of that organization. He is also a glider pilot and a flight instructor with the Penn State Soaring Club.

Selected Publications[4] Edit

  • Kody, F., Corle, E., Maughmer, M., and S. Schmitz. 2016. Higher-Harmonic Deployment of Trailing-Edge Flaps for Rotor-Performance Enhancement and Vibration Reduction. Journal of Aircraft Vol. 53(2) pp. 333–342.
  • Coder, J. G. and M. D. Maughmer. 2014. CFD Compatible Transition Modeling Using an Amplification Factor Transport Equation. AIAA Journal Vol. 52(11) pp. 2506–2512.
  • Coder, J.G., Maughmer, M.D., and D. M. Somers, D.M. 2014. Theoretical and Experimental Results for the S414, Slotted, Natural-Laminar-Flow Airfoil. Journal of Aircraft Vol. 51(6) pp. 1883–1890.
  • Cole, J.A., Vieira, B.A.O., Coder, J.G., Premi, A., and M.D. Maughmer. 2013. An Experimental Investigation into the Effects of Gurney Flaps on Various Airfoils. Journal of Aircraft Vol. 50(4) pp. 1287–1294.
  • Bramesfeld, G. and M. D. Maughmer. 2008. A Free-Wake, Lifting-Surface Model Using Distributed Vorticity Elements. Journal of Aircraft Vol. 45(2) pp. 560–568.
  • Maughmer, M., Lesieutre, G., and M.P. Kinzel. 2007. Miniature Trailing-Edge Effectors for Rotorcraft Performance Enhancement. Journal of the American Helicopter Society Vol. 52(2) pp. 146–158.
  • Bramesfeld, G., Maughmer, M.D., and S. M. Willits. 2006. Piloting Strategies for Controlling a Transport Aircraft after Vertical-Tail Loss. Journal of Aircraft Vol. 43(1) pp. 216–225.
  • M.D. Maughmer. 2003. The Design of Winglets for High-Performance Sailplanes. Journal of Aircraft Vol. 40(6) pp. 1099–1106.
  • Maughmer, M.D., Swan, T.J., and S. M.Willits. 2002. The Design and Testing of a Winglet Airfoil for Low-Speed Aircraft. Journal of Aircraft Vol. 39(4) pp. 654–661.
  • Selig, M.S., Maughmer, M.D., and D. M. Somers. 1995. A Natural Laminar Flow Airfoil for General Aviation Applications. Journal of Aircraft Vol. 32(4) pp. 710–715.
  • Dini, P. and M. D. Maughmer. 1994. A Locally Interactive Laminar Separation Bubble Model. Journal of Aircraft Vol. 31(4) pp.  802–810.
  • Maughmer, M., L. Ozoroski, D. Straussfogel, and L. Long. 1993. Validation of Engineering Methods for Predicting Hypersonic Vehicle Controls Forces and Moments. Journal of Guidance, Control and Dynamics Vol. 16(4) pp. 762–769.
  • Selig, M. S., and M. D. Maughmer. 1992. Generalized Multi-Point Inverse Airfoil Design. AIAA Journal, Vol. 30(11) pp. 2618–2615.
  • Dini, P., M. S. Selig, and M. D. Maughmer. 1992. A Simplified Transition Prediction Method for Separated Boundary Layers. AIAA Journal Vol. 30(8) pp. 1953–1961.
  • Maughmer, M. D., and D. M. Somers. 1989. Design and Experimental Results for a High-Altitude, Long-Endurance Airfoil. Journal of Aircraft Vol. 26(2) pp. 148–153.
  • Ormsbee, A.I. and M. D. Maughmer. 1986. A Class of Airfoils Having Finite Trailing Edge Pressure Gradients. Journal of Aircraft Vol. 23(2) pp. 97–103.
  • Ormsbee, A.I., Bragg, M.B., Maughmer, M.D., and F.L. Jordan. 1981. Scaling Wake-Particle Interactions for Aerial Applications Research. Journal of Aircraft Vol. 18(7) pp. 592–596.

References Edit

  1. ^ Groen Brothers Aviation Consultant Resumes 2007-02-05 at the Wayback Machine. Accessed January 3, 2007.
  2. ^ Masak, Peter (Apr–May 1992). "Winglet Design for Sailplanes" (PDF). Free Flight. 1992 (2): 8. ISSN 0827-2557. Retrieved 2006-01-07.
  3. ^ The tip of the iceberg by Curtis Chan, In: Engineering Penn State Magazine, Summer 2000. 2011-07-18 at the Wayback Machine. Accessed 2010-09-01
  4. ^ "Mark D. Maughmer".

External links Edit

  • Prof. Maughmer's page at Penn State
  • About Winglets paper by Mark D. Maughmer
  • at the Wayback Machine (archived June 18, 2006) paper by Mark D. Maughmer and Peter J. Kunz

mark, maughmer, born, january, 1950, professor, aerospace, engineering, department, aerospace, engineering, pennsylvania, state, university, widely, published, author, known, throughout, world, leading, aerodynamicists, especially, areas, airfoil, winglet, des. Mark D Maughmer born January 18 1950 is a professor of Aerospace Engineering in the Department of Aerospace Engineering at The Pennsylvania State University He is a widely published author known throughout the world as one of the leading aerodynamicists especially in the areas of airfoil and winglet design and analysis wing optimization natural laminar flow aerodynamics and subsonic low turbulence wind tunnel design and operation 1 Mark D MaughmerAlma materUniversity of Illinois 1983Known forAerodynamics Winglet DesignScientific careerInstitutionsPennsylvania State University Contents 1 Winglets 2 Education and academics 3 Selected Publications 4 4 References 5 External linksWinglets Edit PSU 90 125 winglet airfoil profileIn 1987 Peter Masak called on Maughmer about designing winglets for his sailplane to improve performance Others had attempted to apply Richard T Whitcomb s NASA winglets to gliders and though they did improve climb performance this did not offset the parasite drag penalty in high speed cruise Masak was convinced it was possible to overcome this hurdle and Maughmer was willing to join his quest By trial and error they ultimately developed successful winglet designs for gliding competitions and at the 1991 World Gliding Championships in Uvalde Texas the trophy for the highest speed went to a winglet equipped 15 meter class limited wingspan glider exceeding the highest speed in the unlimited span Open Class an exceptional result 2 The winglets were originally retrofit to production sailplanes but now most high performance gliders are equipped from the factory with winglets or some other wingtip device 3 Maughmer has consulted with German sailplane designers on winglets non planar wing tips and other aerodynamic improvements incorporated in several production sailplanes citation needed Education and academics EditThis section of a biography of a living person does not include any references or sources Please help by adding reliable sources Contentious material about living people that is unsourced or poorly sourced must be removed immediately Find sources Mark D Maughmer news newspapers books scholar JSTOR May 2019 Learn how and when to remove this template message He received his Ph D Aeronautical and Astronautical Engineering from the University of Illinois in 1983 M S from Princeton University in 1975 and B S from the University of Illinois in 1972 Maughmer received the PSES Outstanding Teaching Award in 1993 the PSES Premier Teaching Award in 2001 and the Alumni Faculty Teaching Fellow Award in 2012 In 2009 Maughmer received the ASEE Fred Merryfield Design Award a national award for teaching excellence in engineering design He is active in the AIAA and has served on the Aircraft Design Technical Committee 1987 90 He received the AIAA ASEE John Leland Atwood Award in 2013 and the AIAA William T Piper Award in 2014 For the Soaring Society of America he is chair of configuration and design for the Technical Board serves on the board of directors for the Collegiate Soaring Association and received the society s Exceptional Service Award in 1991 He has served on the Board of the International Organization for the Science and Technology of Soaring OSTIV and is currently the vice president of that organization He is also a glider pilot and a flight instructor with the Penn State Soaring Club Selected Publications 4 EditKody F Corle E Maughmer M and S Schmitz 2016 Higher Harmonic Deployment of Trailing Edge Flaps for Rotor Performance Enhancement and Vibration Reduction Journal of Aircraft Vol 53 2 pp 333 342 Coder J G and M D Maughmer 2014 CFD Compatible Transition Modeling Using an Amplification Factor Transport Equation AIAA Journal Vol 52 11 pp 2506 2512 Coder J G Maughmer M D and D M Somers D M 2014 Theoretical and Experimental Results for the S414 Slotted Natural Laminar Flow Airfoil Journal of Aircraft Vol 51 6 pp 1883 1890 Cole J A Vieira B A O Coder J G Premi A and M D Maughmer 2013 An Experimental Investigation into the Effects of Gurney Flaps on Various Airfoils Journal of Aircraft Vol 50 4 pp 1287 1294 Bramesfeld G and M D Maughmer 2008 A Free Wake Lifting Surface Model Using Distributed Vorticity Elements Journal of Aircraft Vol 45 2 pp 560 568 Maughmer M Lesieutre G and M P Kinzel 2007 Miniature Trailing Edge Effectors for Rotorcraft Performance Enhancement Journal of the American Helicopter Society Vol 52 2 pp 146 158 Bramesfeld G Maughmer M D and S M Willits 2006 Piloting Strategies for Controlling a Transport Aircraft after Vertical Tail Loss Journal of Aircraft Vol 43 1 pp 216 225 M D Maughmer 2003 The Design of Winglets for High Performance Sailplanes Journal of Aircraft Vol 40 6 pp 1099 1106 Maughmer M D Swan T J and S M Willits 2002 The Design and Testing of a Winglet Airfoil for Low Speed Aircraft Journal of Aircraft Vol 39 4 pp 654 661 Selig M S Maughmer M D and D M Somers 1995 A Natural Laminar Flow Airfoil for General Aviation Applications Journal of Aircraft Vol 32 4 pp 710 715 Dini P and M D Maughmer 1994 A Locally Interactive Laminar Separation Bubble Model Journal of Aircraft Vol 31 4 pp 802 810 Maughmer M L Ozoroski D Straussfogel and L Long 1993 Validation of Engineering Methods for Predicting Hypersonic Vehicle Controls Forces and Moments Journal of Guidance Control and Dynamics Vol 16 4 pp 762 769 Selig M S and M D Maughmer 1992 Generalized Multi Point Inverse Airfoil Design AIAA Journal Vol 30 11 pp 2618 2615 Dini P M S Selig and M D Maughmer 1992 A Simplified Transition Prediction Method for Separated Boundary Layers AIAA Journal Vol 30 8 pp 1953 1961 Maughmer M D and D M Somers 1989 Design and Experimental Results for a High Altitude Long Endurance Airfoil Journal of Aircraft Vol 26 2 pp 148 153 Ormsbee A I and M D Maughmer 1986 A Class of Airfoils Having Finite Trailing Edge Pressure Gradients Journal of Aircraft Vol 23 2 pp 97 103 Ormsbee A I Bragg M B Maughmer M D and F L Jordan 1981 Scaling Wake Particle Interactions for Aerial Applications Research Journal of Aircraft Vol 18 7 pp 592 596 References Edit Groen Brothers Aviation Consultant Resumes Archived 2007 02 05 at the Wayback Machine Accessed January 3 2007 Masak Peter Apr May 1992 Winglet Design for Sailplanes PDF Free Flight 1992 2 8 ISSN 0827 2557 Retrieved 2006 01 07 The tip of the iceberg by Curtis Chan In Engineering Penn State Magazine Summer 2000 Archived 2011 07 18 at the Wayback Machine Accessed 2010 09 01 Mark D Maughmer External links EditProf Maughmer s page at Penn State About Winglets paper by Mark D Maughmer Sailplane Winglet Design at the Wayback Machine archived June 18 2006 paper by Mark D Maughmer and Peter J Kunz Retrieved from https en wikipedia org w index php title Mark D Maughmer amp oldid 1122906280, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.