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Volumn 28, Issue 6, 2007, Pages 1312-1317

Stability features of low aspect-ratio flying wings

Author keywords

Dutch roll mode; Flying wing; Low aspect ratio; Short period mode; Stability

Indexed keywords

ANGLE OF ATTACK; ASPECT RATIO; CONTROL SYSTEMS; FIGHTER AIRCRAFT; STABILITY;

EID: 37449023960     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (20)

References (17)
  • 1
    • 0003528698 scopus 로고    scopus 로고
    • Modular control design for the innovative control effectors (ICE) tailless fighter aircraft configuration
    • AFRL-VA-WP-TR-1999-3057
    • Buffington J M. Modular control design for the innovative control effectors (ICE) tailless fighter aircraft configuration [R]. AFRL-VA-WP-TR-1999-3057, 1999: 9-147.
    • (1999) , pp. 9-147
    • Buffington, J.M.1
  • 3
    • 84959093854 scopus 로고    scopus 로고
    • Linear parameter varying control for a tail less aircraft
    • AIAA-97-3636
    • Sparks A G. Linear parameter varying control for a tail less aircraft [R]. AIAA-97-3636, 1997: 1035-1043.
    • (1997) , pp. 1035-1043
    • Sparks, A.G.1
  • 4
    • 71449089028 scopus 로고    scopus 로고
    • Sliding mode control for tailless aircraft
    • AIAA-97-3633
    • Tournes C, Shtessel Y B. Sliding mode control for tailless aircraft [R]. AIAA-97-3633, 1997: 1299-1309.
    • (1997) , pp. 1299-1309
    • Tournes, C.1    Shtessel, Y.B.2
  • 5
    • 19944392826 scopus 로고    scopus 로고
    • Control-surface deflection effects on the innovative control effectors (ICE 101) design
    • AFRL-VA-WP-TR-2000-3027
    • Addington G A, Myatt J H. Control-surface deflection effects on the innovative control effectors (ICE 101) design [R]. AFRL-VA-WP-TR-2000-3027, 2000: 2-175.
    • (2000) , pp. 2-175
    • Addington, G.A.1    Myatt, J.H.2
  • 6
    • 66149142429 scopus 로고    scopus 로고
    • Innovative control effectors (configuration 101) dynamic wind tunnel test report
    • AFRL VA-WP-TR 1998-3043
    • Gillard W J. Innovative control effectors (configuration 101) dynamic wind tunnel test report [R]. AFRL VA-WP-TR 1998-3043, 1998: 1-196.
    • (1998) , pp. 1-196
    • Gillard, W.J.1
  • 7
    • 37449029220 scopus 로고    scopus 로고
    • Beijing: Beijing University of Aeronautics and Astronautics Press. Chinese source
    • Fang Zhenping, Chen Wanchun, Zhang Shuguang. Aircraft flight dynamics [M]. Beijing: Beijing University of Aeronautics and Astronautics Press. 2005: 206. (in Chinese)
    • (2005) Aircraft Flight Dynamics , pp. 206
    • Fang, Z.1    Chen, W.2    Zhang, S.3
  • 8
    • 37449016140 scopus 로고    scopus 로고
    • Flight control using distributed shape-change effector arrays
    • AIAA 2000 1560
    • David L R, Raymond C M, Lawrence L G, et al. Flight control using distributed shape-change effector arrays [R]. AIAA 2000 1560, 2000: 6-8.
    • (2000) , pp. 6-8
    • David, L.R.1    Raymond, C.M.2    Lawrence, L.G.3
  • 10
    • 37449026147 scopus 로고    scopus 로고
    • The development of all-wing aircraft
    • Northrop J K. The development of all-wing aircraft [EB/OL]. http://www.nurflugel.com/ Nurflugel/Northrop/Northrop_address/body_northrop_address.html.
    • Northrop, J.K.1
  • 11
    • 37449004511 scopus 로고    scopus 로고
    • Airfoils for tailless airplanes: Design and selection
    • Hepperle M. Airfoils for tailless airplanes: design and selection [EB/OL]. http://www.mh-aerotools.de/airfoils/nf_1.htm.
    • Hepperle, M.1
  • 12
    • 37449033403 scopus 로고    scopus 로고
    • Dynamics and control of tailless aircraft
    • AIAA-97-3776
    • Ralph P, William G L. Dynamics and control of tailless aircraft [R]. AIAA-97-3776, 1997: 725-732.
    • (1997) , pp. 725-732
    • Ralph, P.1    William, G.L.2
  • 13
    • 0003505351 scopus 로고
    • Tailless aircraft in theory and practice
    • Washington, DC: American Institute of Aeronautics and Astronautics
    • Nickel K, Wohlfahrt M. Tailless aircraft in theory and practice [M]. Washington, DC: American Institute of Aeronautics and Astronautics, 1994: 117-120.
    • (1994) , pp. 117-120
    • Nickel, K.1    Wohlfahrt, M.2
  • 14
    • 24744432346 scopus 로고
    • Aerodynamic characteristics analysis and engineering calculation of flight aircraft
    • Xi'an: Northwestern Polytechnical University Press, Chinese source
    • Yan Hengyuan. Aerodynamic characteristics analysis and engineering calculation of flight aircraft [M]. Xi'an: Northwestern Polytechnical University Press, 1990: 203-211. (in Chinese)
    • (1990) , pp. 203-211
    • Yan, H.1
  • 15
    • 11144229733 scopus 로고    scopus 로고
    • Beijing: Beijing University of Aeronautics and Astronautics Press, Chinese source
    • Gu Songfen. Aircraft conceptual/preliminary design [M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2001: 49-51. (in Chinese)
    • (2001) Aircraft Conceptual/Preliminary Design , pp. 49-51
    • Gu, S.1
  • 16
    • 37449030063 scopus 로고    scopus 로고
    • Beijing: Aviation Industry Press, Chinese source
    • Fang Baorui. Aircraft aerodynamics configuration design [M]. Beijing: Aviation Industry Press, 1997: 779-799. (in Chinese)
    • (1997) Aircraft Aerodynamics Configuration Design , pp. 779-799
    • Fang, B.1
  • 17
    • 34249869331 scopus 로고    scopus 로고
    • Numerical research on roll and sideslip coupling motions about a slender delta-wing
    • Chinese source
    • Yang Yunjun, Cui Erjie, Zhou Weijiang. Numerical research on roll and sideslip coupling motions about a slender delta-wing [J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(1): 14-19. (in Chinese)
    • (2007) Acta Aeronautica et Astronautica Sinica , vol.28 , Issue.1 , pp. 14-19
    • Yang, Y.1    Cui, E.2    Zhou, W.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.