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Volumn 2, Issue , 2005, Pages 952-960

Second generation inflatable/rigidizable wings for low-density flight applications

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPOSITE MATERIALS; FLIGHT DYNAMICS; OPTIMIZATION; PARACHUTES; PRESSURIZATION; STRESS ANALYSIS;

EID: 28844469969     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1883     Document Type: Conference Paper
Times cited : (18)

References (9)
  • 1
    • 85086488803 scopus 로고    scopus 로고
    • The design of the canyon flyer, an airplane for mars exploration
    • AIAA Paper 2000-0514, Reno NV, January
    • Smith, S.C., et al., "The Design of the Canyon Flyer, an Airplane for Mars Exploration," AIAA Paper 2000-0514, AIAA Aerospace Sciences Meeting, Reno NV, January 2000.
    • (2000) AIAA Aerospace Sciences Meeting
    • Smith, S.C.1
  • 3
    • 84861295741 scopus 로고    scopus 로고
    • April 13
    • http://marsairplane.larc.nasa.gov/, April 13, 2005.
    • (2005)
  • 9
    • 0024552399 scopus 로고
    • XFOIL: An analysis and design system for low reynolds number airfoils
    • Low Reynolds Number Aerodynamics. T.J. Mueller (Editor). Springer Verlag
    • Drela, M. "XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils." Low Reynolds Number Aerodynamics. T.J. Mueller (Editor). Lecture Notes in Engineering No. 54, Springer Verlag, 1989.
    • (1989) Lecture Notes in Engineering No. 54 , vol.54
    • Drela, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.