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Volumn 67, Issue , 1996, Pages 176-183

Nonlinear dynamics of a vectored thrust aircraft

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EID: 0038199703     PISSN: 02811847     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1088/0031-8949/1996/t67/034     Document Type: Article
Times cited : (15)

References (30)
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  • 7
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    • Anaheim, Sept. 18-23
    • Baxter, J. S. and Sweeney, J. E., "Development and Flight Test of a Multi-Axis Thrust Vectoring System for the F-16", presented at the 19th CAS Conf. Anaheim, Sept. 18-23, 1994.
    • (1994) 19th CAS Conf.
    • Baxter, J.S.1    Sweeney, J.E.2
  • 8
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    • (1989) Interavia , pp. 806-807
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    • December 6
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  • 11
    • 0346517956 scopus 로고
    • The Effect of Nonlinearities on Thrust Vectoring
    • Anaheim, Sept. 18-23
    • Gránásy, P., "The Effect of Nonlinearities on Thrust Vectoring", 19th CAS Conf. Anaheim, Sept. 18-23, 1994, p. 2663-2668.
    • (1994) 19th CAS Conf. , pp. 2663-2668
    • Gránásy, P.1
  • 14
    • 0028195691 scopus 로고
    • Application of Bifurcation Theory to the High-Angle-of-Attack Dynamics of F-14
    • Jahnke, C. C. and Culick, F. E. C., "Application of Bifurcation Theory to the High-Angle-of-Attack Dynamics of F-14", J. Aircraft 31, 26 (1994).
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    • Jahnke, C.C.1    Culick, F.E.C.2
  • 19
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    • Longman Scientific and Technical
    • Barnard, R. H., "Aircraft Flight" (Longman Scientific and Technical 1995).
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    • April
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    • (1977) J. Aircraft , pp. 375-382
    • Schy, A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.