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Volumn 8, Issue , 2006, Pages 5422-5438

Developing morphing wing weight predictors with emphasis on the actuating mechanism

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATOR WEIGHTS; MORPHING AIRCRAFT; RESPONSE SURFACE METHODS; WING WEIGHT EQUATIONS;

EID: 34147184318     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (20)
  • 3
    • 16244422395 scopus 로고    scopus 로고
    • Darpa Eyes Materials for 'Morphing' Aircraft
    • April 8
    • Wall, R., "Darpa Eyes Materials for 'Morphing' Aircraft," Aviation Week and Space Technology, April 8, 2002.
    • (2002) Aviation Week and Space Technology
    • Wall, R.1
  • 6
    • 84964445624 scopus 로고
    • Statistical Weight Estimation Methods for Figher/Attack Aircraft
    • Vought Aircraft Rept. 2-59320/8R-50475
    • Staton, R.N., "Statistical Weight Estimation Methods for Figher/Attack Aircraft," Vought Aircraft Rept. 2-59320/8R-50475, 1968.
    • (1968)
    • Staton, R.N.1
  • 9
    • 84983189336 scopus 로고    scopus 로고
    • Balabanoc, V., Kaufman, M. Knill, D. L., Haim, D., Golovidov, O., Guinta, A. A., Haftka, Raphael T., Grossman, B., Mason, W. H., and Watson, L. T., Dependence of Optimal Structural Weight on Aerodynamic Shape for a High Speed Civil Transport, AIAA 1996-4046, NASA, and ISSMO, Symposium on Multidisciplinary Analysis and Optimization, 6th. Bellevue, WA, Sept. 4-6, 1996, Technical Papers. Pt. 1 (A96-38701 10-31)
    • Balabanoc, V., Kaufman, M. Knill, D. L., Haim, D., Golovidov, O., Guinta, A. A., Haftka, Raphael T., Grossman, B., Mason, W. H., and Watson, L. T., "Dependence of Optimal Structural Weight on Aerodynamic Shape for a High Speed Civil Transport," AIAA 1996-4046, NASA, and ISSMO, Symposium on Multidisciplinary Analysis and Optimization, 6th. Bellevue, WA, Sept. 4-6, 1996, Technical Papers. Pt. 1 (A96-38701 10-31)
  • 11
    • 34147180971 scopus 로고    scopus 로고
    • Developing Response Surface based Wing Weight Equations for Conceptual Morphing Aircraft Sizing,
    • MS Thesis, School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN, Dec
    • Skillen, M., "Developing Response Surface based Wing Weight Equations for Conceptual Morphing Aircraft Sizing," MS Thesis, School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN, Dec. 2005.
    • (2005)
    • Skillen, M.1
  • 18
    • 34147174793 scopus 로고    scopus 로고
    • Morphing Aircraft Structures, DARPA Defense Sciences Office, [http://www.darpa.mil/dso/thrust/matdev/mas.htm], accessed Jan. 2006.
    • "Morphing Aircraft Structures," DARPA Defense Sciences Office, [http://www.darpa.mil/dso/thrust/matdev/mas.htm], accessed Jan. 2006.
  • 19
    • 0142231859 scopus 로고    scopus 로고
    • Flying on Flexible Wings
    • November
    • Ahsley, S., "Flying on Flexible Wings," Scientific American, November 2003, pp. 84-91.
    • (2003) Scientific American , pp. 84-91
    • Ahsley, S.1
  • 20
    • 16244401016 scopus 로고    scopus 로고
    • ASTROS, Torrance, CA, Universal Analytics, Inc
    • ASTROS Theoretical Manual for Version 20. Torrance, CA, Universal Analytics, Inc. 1997.
    • (1997) Theoretical Manual for Version 20


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.