This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Design Drivers of Energy-Efficient Transport Aircraft

Journal Article
ISSN: 1946-3855, e-ISSN: 1946-3901
Published October 18, 2011 by SAE International in United States
Design Drivers of Energy-Efficient Transport Aircraft
Citation: Drela, M., "Design Drivers of Energy-Efficient Transport Aircraft," SAE Int. J. Aerosp. 4(2):602-618, 2011,
Language: English


  1. NASA Aeronautics Research Mission Directorate Fundamental Aeronatics Program: Subsonic Fixed Wing Sep 2009
  2. NASA Aeronautics Research Mission Directorate N+3 Program June 2010
  3. Hileman, J.I Katz, J.B. Mantilla, J. Fleming, G. Pay- load fuel energy efficiency as a metric for aviation environmental performance Proceedings of the 26th IGAS Conference Anchorage, AK Sep 2008
  4. Shevell, R.S. Fundamentals of Flight 2nd Edition Prentice Hall EngleWood Cliffs, New Jersey 1989
  5. Bushnell, D.M. Aircraft drag reduction - a review Journal of Aerospace Engineering 217 1 18 2003
  6. Roskam, J. Airplane Design DAR Corporation Lawrence, Kansas 2000
  7. Torrenbeek, E. Synthesis of Subsonic Airplane Design Delft University Press 1988
  8. Raymer, D.P. Aircraft Design: A Conceptual Approach AIAA Education AIAA 1992
  9. Jayaram, S. Myklebust, A. Gelhausen, P. ACSYNT - A standards-based system for parametric computer aided conceptual design of aircraft AIAA Paper 92-1268 Feb 1992
  10. Mason, W.H. Arledge, T.K. ACSYNT aerodynamic estimation - An examination and validation for use in conceptual design AIAA Paper 93-0973 Feb 1993
  11. Knapp, M.B. Applications of a nonlinear wing planform design program Master's thesis MIT Aug 1996
  12. Wakayama, S. Lifting Surface Design Using Multidisci- plinary Optimization PhD thesis Stanford June 1994
  13. Kroo, I. PASS, Program for Aircraft Synthesis Studies Software Package Desktop Aeronautics Palo Alto, CA 2005
  14. Drela, M. N+3 Aircraft Concept Designs and Trade Studies - Appendix Technical Report NASA CR-2010- 216794/VOL2 NASA 2010
  15. Greitzer, E.G. N+3 Aircraft Concept Designs and Trade Studies: Technical Report NASA CR-2010-216794/VOL1 NASA 2010
  16. Chang, F. Structural health monitoring; The demands and challenges CRC Press 1999
  17. Koff, B.L. Gas turbine technology evolution: A designer's perspective Journal of Propusion and Power 20 4 577 595 Jul Aug 2004
  18. NASA Glenn Research Center Ultra-Efficient Engine Technology Program Jan 2010
  19. Sliwa, S.M. Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability Technical Report TP-1980-1760 NASA 1980
  20. Liu, S.J. Kline, C.K. Johnston, J.P. An experimental study of turbulent boundary layer on rough walls Report MD-15 Stanford U. Dep. Mech. Eng. July 1966
  21. McLean, J.D. George-Falvy, D.N. Sullivan, P.P Flight- test of turbulent skin friction reduction by riblets Proceedings of International Conference on Turbulent Drag Reduction by Passive Means Royal Aeronautical Society London 1987
  22. Reed, H.L. Saric, D. Arnal, W.S. Linear stability theory applied to boundary layers Annual Reviews of Fluid, Mechanics 28 1996
  23. Boeing Commercial Aircraft Group High reynolds number hybrid laminar flow control (HLFC) flight experiment Technical Report CR-1999-209324 NASA 1999
  24. Joslin, R.D. Overview of laminar flow control Technical Report TP-199&-208705 NASA 1998
  25. Fujino, M. Yoshizaki, Y. Kawamura, Y. Natural laminar-flow airfoil development for a lightweight business jet Journal of Aircraft 40 4 609 615 Jul Aug 2003
  26. Liebeck, R. Design of the Blended Wing Body subsonic transport Journal of Aircraft 41 1 Jan 2004
  27. McMasters, J.H. Kroo, I. Advanced configurations for very large subsonic transport airplanes Technical Memorandum TM 109154 NASA Sept 1994
  28. Wolkovitch, J. The joined wing: An overview Journal of Aircraft 23 3 Mar 1986
  29. Pfenninger, W. Some thoughts on the design of large global range lfc transport airplanes Special Course on Concepts for Drag Reduction AGARD 1976
  30. Drela, M. Development of the D8 Transport Configuration AIAA Paper 2011-3970 June 2011
  31. Gur, O. Bhatia, M. Mason, W.H. Schetz, J.A. Kapania, R.K. Nam, T. Development of a framework for truss-braced wing conceptual MDO Struc. Multidic. Optim. 44 277 298 2011 AIAA paper 2010-2754

Cited By