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Volumn , Issue , 1996, Pages

Development of a nonlinear indicial model for maneuvering fighter aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ANGLE OF ATTACK; MANEUVERABILITY; SUPERSONIC AIRCRAFT;

EID: 17444383268     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (15)

References (23)
  • 9
    • 0019000414 scopus 로고    scopus 로고
    • Approximate Analysis of Nonlinear Systems by Laplace Transform
    • Kannakar, S. B.: Approximate Analysis of Nonlinear Systems by Laplace Transform, J. Sound and Vib., Vol. 69, No. 4, pp. 597-602.
    • J. Sound and Vib , vol.69 , Issue.4 , pp. 597-602
    • Kannakar, S.B.1
  • 15
    • 0028498390 scopus 로고
    • State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack
    • Goman, M. and Khrabrov, A.: State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack, J. Aircraft, Vol. 31, No. 5, 1994, pp. 1109-1115.
    • (1994) J. Aircraft , vol.31 , Issue.5 , pp. 1109-1115
    • Goman, M.1    Khrabrov, A.2
  • 16
    • 0023436856 scopus 로고
    • Lift-Curve Characteristics for an Airfoil Pitching at Constant Rate
    • Jumper, E. J., Schreck, S. J., and Dimmick, R. L.: Lift-Curve Characteristics for an Airfoil Pitching at Constant Rate, J. Aircraft, Vol. 24, No. 10, 1987, pp. 680-687.
    • (1987) J. Aircraft , vol.24 , Issue.10 , pp. 680-687
    • Jumper, E.J.1    Schreck, S.J.2    Dimmick, R.L.3
  • 17
    • 84962192732 scopus 로고
    • Experimental Investigation of Delta Wing A = 1. 5 Damping in Roll and Pitch at High Angles of Attack
    • Moscow
    • Ioselevich, A. S., Stolyarov, G. I., Tabachnikov, V. G., and Zhuk, A. N.: Experimental Investigation of Delta Wing A = 1. 5 Damping in Roll and Pitch at High Angles of Attack, Proceedings of the TsAGI, Issue 2290, Moscow, 1985, pp. 52-7O.
    • (1985) Proceedings of the TsAGI , Issue.2290 , pp. 52-70
    • Ioselevich, A.S.1    Stolyarov, G.I.2    Tabachnikov, V.G.3    Zhuk, A.N.4
  • 18
    • 85003260064 scopus 로고
    • Cobra Maneuver Unsteady Aerodynamic Considerations
    • Ericsson, L. E.: Cobra Maneuver Unsteady Aerodynamic Considerations, J. Aircraft, Vol. 32, No. 1, 1995, pp. 214-216.
    • (1995) J. Aircraft , vol.32 , Issue.1 , pp. 214-216
    • Ericsson, L.E.1
  • 20
    • 0029167337 scopus 로고
    • Effects of Initial Acceleration on the Flow Field Development Around Rapidly Pitching Airfoils
    • March
    • Gendrich, C. P., Koochesfahani, M. M., and Visbal, M. R.: Effects of Initial Acceleration on the Flow Field Development Around Rapidly Pitching Airfoils, J. Fluids Engineering, March 1995, Vol. 117, pp. 45-49.
    • (1995) J. Fluids Engineering , vol.117 , pp. 45-49
    • Gendrich, C.P.1    Koochesfahani, M.M.2    Visbal, M.R.3
  • 21
    • 0024902625 scopus 로고
    • Theoretical Description of Transient Stimulated Raman Scattering in Optical Fibers
    • December
    • Blow, K. J. and Wood, D.: Theoretical Description of Transient Stimulated Raman Scattering in Optical Fibers, IEEE J. Quantum Electronics, Vol. 25, No. 12, December 1989, pp. 2665-2673.
    • (1989) IEEE J. Quantum Electronics , vol.25 , Issue.12 , pp. 2665-2673
    • Blow, K.J.1    Wood, D.2
  • 22
    • 84962201890 scopus 로고    scopus 로고
    • Algorithm 660, Collected Algorithms from ACM
    • Algorithm 660, Collected Algorithms from ACM, Transactions on Mathematical Software, Vol. 14, No. 2, p. 149.
    • Transactions on Mathematical Software , vol.14 , Issue.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.