Edmund W. Pendleton

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Edmund W. Pendleton is an American research and development engineer, commercial pilot, and flight instructor best known for his work on the X-53 flight research program. He joined the United States Air Force Research Laboratory in Dayton, Ohio in 1980. While employed there, he conducted wind tunnel research[1][2][3] leading up to the Grumman X-29, the X-30 National Aerospace Plane, and the X-53 aircraft programs. He was one of the original developers of the active aeroelastic wing concept,[4][5] a novel engineering design approach that utilized wing aeroelastic twist to control aircraft at high speeds. He served as a program manager and chief engineer of the X-53 Active Aeroelastic Wing flight research program from 1992 through 2005.[6][7] The Active Aeroelastic Wing project received a NASA "Turning Goals into Reality Award" in 2004.[8] Mr Pendleton was also active in quantifying the effects of aerodynamics on the twin tails of fighter aircraft[9] .[10]

Ed Pendleton attended grade school in Wayne Township, Ohio.[11] After transferring, he graduated from Beavercreek High School, Xenia Ohio, where he played on the school's basketball and baseball teams from 1972-1975[12][13] After service in the U.S. army, Ed Pendleton earned his bachelor’s degree in systems engineering from Wright State University in Fairborn, Ohio in 1979 [14] and a commercial pilot's licence in 1981.[15]

He earned a master’s degree in aerospace engineering from the University of Dayton[16] in Ohio and his flight instructor’s certification in 1984.[17][18] In 1998, Ed graduated from the Defense Systems Management College’s Advanced Program Manager’s Course.[19] In 2003, Ed earned a master’s degree in national security strategy from the National Defense University located in Washington DC.[20]

In 2005, he became involved in efforts to provide technology for an initiative entitled "Operationally Responsive Space". From 2006 through 2011, he has served as a project manager/engineer for an air/spaceframe development effort involving the integration of a low mass fraction, load bearing, cryogenic, composite, linerless fuel and oxidizer tank with lifting surfaces, thermal protection, and condition based maintenance under a Future Responsive Access to Space Technology initiative.[21][22][23][24][25][26][27] This initiative will pave the way for increased the structural efficiency of future Space Launch Vehicles.

Ed served for ten years on a NATO technical panel for aerospace structures and materials where he coauthored several papers.[28]

Ed Pendleton has been a registered Professional Engineer in the State of Ohio since 1984.[29][30]

Notes

  1. ↑ Hertz, T. and Pendleton, E., "The Effect of Stores Carriage on Body-Freedom Flutter,",Proceedings of the AGARD Fluid Dynamics Panel Symposium on Store-Airframe Aerodynamics Fall 1985, Athens, Greece, October 1985.
  2. ↑ Pendleton, E., Lee, M., and Wasserman, L., "A Low Speed Flexible Model Simulating an F-16 Derivative Wing Design," WRDC TR-90-3083, Dayton, Ohio, January 1990.
  3. ↑ Pendleton, E., Moster, G., and Keller, D., "Transonic Aeroelastic Models of Hypersonic Highly Swept Lifting Surfaces," Journal of Aircraft, Volume 32, Number 6, November–December 1995.
  4. ↑ Pendleton, E., Lee, M., and Wasserman, L., "A Low Speed Flexible Model Simulating an F-16 Derivative Wing Design," WRDC TR-90-3083, Dayton, Ohio, January 1990.
  5. ↑ Miller, G., "Active Flexible Wing Technology," WRDC TR-87-3096, Los Angeles, California, February 1988.
  6. ↑ Pendleton, E., Bessette, D., Field P., Miller, G., and Griffin, K., "Active Aeroelastic Wing Flight Research Program: Technical Program & Model Analytical Development ," Journal of Aircraft, Volume 37, Number 4, July–August, 2000.
  7. ↑ Pendleton, E., "Active Aeroelastic Wing,” AFRL Technology Horizons, Selected Science and Technology Articles, Vol. 1, No. 2, June 2000.
  8. ↑ http://www.aeronautics.nasa.gov/events/tgir/2004/2004_award_winners.pdf
  9. ↑ Pettit, C., Brown, D., Banford, M., and Pendleton, E., "Full Scale Wind Tunnel Pressure Measurements of an F/A-18 Tail During Buffet," Journal of Aircraft , Volume 33, Number 6, Pages 1148-1156, December 1996.
  10. ↑ Moses, R. and Pendleton, E., "A Comparison of Pressure Measurements Between a Full Scale and a 1/6 Scale F/A-18 Twin Tail During Buffet," Proceedings of the AGARD Structures and Materials Panel, Loads and Requirements for Military Aircraft Workshop, Fall 1996, Florence, Italy, September 1996.
  11. ↑ Wayne High School Yearbook, 1972, Freshman Class, Wayne Township, Ohio
  12. ↑ Beavercreek High School Yearbook, 1975, Beavercreek, Ohio
  13. ↑ Dayton Daily News Sports Section, Dec. 1974.
  14. ↑ Wright State University, Fairborn, Ohio transcript archives
  15. ↑ https://amsrvs.registry.faa.gov/airmeninquiry/
  16. ↑ University of Dayton, Ohio transcript archives
  17. ↑ Pilot Logbook Records of Ed Pendleton
  18. ↑ https://amsrvs.registry.faa.gov/airmeninquiry/
  19. ↑ DSMC transcript records, Ft Belvoir, Virgina
  20. ↑ D.C.Buck, Col. D., Spacey, Col. W., Pendleton, Mr. E., et al., “Space Industry Study Final Report, Spring 2003," The Industrial College of the Armed Forces, National Defense University, Washington DC, June 2003
  21. ↑ Pendleton, E., Zweber, J., and Johnson, R.G., “A Technology Readiness Assessment for Affordable, Responsive Hybrid Launch Vehicles,” AFRL-VA-WP-TR-2006-3198, October 2006.
  22. ↑ Griffin, K, and Pendleton, E.,” A Hybrid Launch Vehicle Design Concept Based on Recent Industry Studies, A Consensus View,” Paper AIAA 2008-1135, Proceedings of the 46th AIAA Aerospace Sciences Meeting, Reno, Nevada, January 7-10, 2008..
  23. ↑ Biggs, R, Love, M. and Pendleton, E. "An Integrated Airframe Experiment For Future Responsive Access To Space Application", AIAA Paper2009-2630, Proceedings of the 50th AIAA Structures, Structural Dynamics, and Materials Conference, Palm Springs, California, May 4–7, 2009.
  24. ↑ McCandless, M., Biggs, R., Zink, S., Pendleton, E., and Griffin, K., “Integrated Composite Structures Design for Future Space Launch Vehicle Airframes,” 2010 National Space & Missile Materials Symposium, Scottsdale, Arizona, June 28–30, 2010.
  25. ↑ Cochran, R., Biggs, R., Zink, S., Pendleton, E., and Griffin, K., “Structural Efficiency of Integrated Composite Structures for Future Space Launch Vehicle Airframe Applications,” AIAA Space 2011 Conference and Exposition, Long Beach, California, September 27–29, 2011.
  26. ↑ Pendleton, E., Biggs, R., Cochran, R., Clark, B., and Griffin, K., “Integrated Composite Structures Demonstration for Future Space Launch Vehicle Airframe Applications”, Paper AIAA-2012-1767 , Proceedings of the 53rd AIAA Structures, Structural Dynamics, and Materials Conference, Honolulu, Hawaii, April 23–26, 2012.
  27. ↑ Chen, P.C., Sarhaddi, D., Pendleton, E., and Lindsley, N., “Parametric Studies for Wing Mounted Fins,” Proceedings from The European Forum on Aeroelasticity and Structural Dynamics, Bristol, United Kingdom, June 24–27, 2013.
  28. ↑ Saff, C., Dumoulin, B, Pendleton, E. et al.,“Qualification and Structural Design Guidelines for Military Unmanned Air Vehicles,” NATO Science and Technology Organization, Paris France, October 31, 2012.
  29. ↑ State of Ohio Board of Engineers and Surveyors Roster
  30. ↑ http://www.peps.ohio.gov/Renewal/RenewalRosters.aspx
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