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Volumn , Issue , 2002, Pages

Aeroelastics, flight mechancs and handling qualities of the MOB BWB configuration

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; COMPUTATIONAL FLUID DYNAMICS; DESIGN; ENGINES; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; OPTIMIZATION; TRANSPORT AIRCRAFT;

EID: 84896099973     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (16)
  • 4
    • 84879023904 scopus 로고    scopus 로고
    • 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, September 2002. AIAA-2002-5448
    • Qin, N., Aerodynamic Studies of Blended Wing Body Aircraft, 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, September 2002. AIAA-2002-5448.
    • Aerodynamic Studies of Blended Wing Body Aircraft
    • Qin, N.1
  • 5
    • 4243103315 scopus 로고    scopus 로고
    • 4.3, ZONA Technology, www.zonatech.com
    • ZAERO Theoretical Manual Ver. 4.3, ZONA Technology, www.zonatech.com
    • ZAERO Theoretical Manual Ver
  • 8
    • 84896082540 scopus 로고    scopus 로고
    • Licentiate Thesis, Report 2002-15, Department of Aeronautics, Kunglika Techniska Högskolan, Stockholm, Sweden, 2002. ISSN 0280-4646
    • Carlsson, M., On the Design and Testing of Aeroelastic Wind Tunnel Models, Licentiate Thesis, Report 2002-15, Department of Aeronautics, Kunglika Techniska Högskolan, Stockholm, Sweden, 2002. ISSN 0280-4646.
    • On the Design and Testing of Aeroelastic Wind Tunnel Models
    • Carlsson, M.1
  • 12
    • 85007685430 scopus 로고
    • A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows
    • February
    • Albano E., Rodden W., A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows, AIAA Journal, Vol. 7, No. 2, February 1969, pp. 279-285.
    • (1969) AIAA Journal , vol.7 , Issue.2 , pp. 279-285
    • Albano, E.1    Rodden, W.2
  • 13
    • 0030289780 scopus 로고    scopus 로고
    • Minimum-State Unsteady Aerodynamic Approximations with Flexible Constraints
    • November-December, Seite
    • Karpel, M., Strul, E., Minimum-State Unsteady Aerodynamic Approximations with Flexible Constraints, Journal of Aircraft, Vol. 33, No. 6, November-December 1996, Seite. 1190-1196.
    • (1996) Journal of Aircraft , vol.33 , Issue.6 , pp. 1190-1196
    • Karpel, M.1    Strul, E.2
  • 16
    • 85088718854 scopus 로고    scopus 로고
    • 10th AIAA/NAL-NASDAISAS International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, April 2001. AIAA-2001-1852
    • Decker, K., Laschka, B., Unsteady Aerodynamics of a Hypersonic Vehicle During a Separation Phase", 10th AIAA/NAL-NASDAISAS International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, April 2001. AIAA-2001-1852.
    • Unsteady Aerodynamics of a Hypersonic Vehicle During a Separation Phase
    • Decker, K.1    Laschka, B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.