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Volumn 28, Issue 3, 2005, Pages 539-540

Longitudinal long-term modes in super- And hypersonic flight

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTATION THEORY; DAMPING; DEFORMATION; EQUATIONS OF MOTION; FLIGHT DYNAMICS; SUBSONIC AERODYNAMICS;

EID: 19644394621     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.5511     Document Type: Article
Times cited : (19)

References (20)
  • 1
    • 0141938631 scopus 로고    scopus 로고
    • Two-timescale analysis of phugoid mode
    • Giulietti, F., "Two-Timescale Analysis of Phugoid Mode," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 5, 2003, pp. 827-830.
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.5 , pp. 827-830
    • Giulietti, F.1
  • 4
    • 0037352113 scopus 로고    scopus 로고
    • Comments on 'literal approximations to aircraft dynamic modes' and 'consistent approximations to aircraft longitudinal modes
    • Mengali, G., "Comments on 'Literal Approximations to Aircraft Dynamic Modes' and 'Consistent Approximations to Aircraft Longitudinal Modes,'" Journal of Guidance, Con-trol, and Dynamics, Vol. 26, No. 2, 2003, pp. 380-383.
    • (2003) Journal of Guidance, Con-trol, and Dynamics , vol.26 , Issue.2 , pp. 380-383
    • Mengali, G.1
  • 7
    • 85008284761 scopus 로고    scopus 로고
    • Comment on does the phugoid frequency depend on speed?
    • Ananthkrishnan, N., "Comment on 'Does the Phugoid Frequency Depend on Speed?,'" Journal of Guidance, Control, and Dynamics, Vol. 23, No. 4, 2000, pp. 765-766.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.4 , pp. 765-766
    • Ananthkrishnan, N.1
  • 8
    • 85008308422 scopus 로고    scopus 로고
    • Reply by author to N. Ananthkrishnan
    • Pradeep, S., "Reply by Author to N. Ananthkrishnan," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 4, 2000, pp. 766, 767.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.4 , pp. 766
    • Pradeep, S.1
  • 9
    • 0033896608 scopus 로고    scopus 로고
    • Phugoid approximation for conventional airplanes
    • Phillips, W. F., "Phugoid Approximation for Conventional Airplanes," Journal of Aircraft, Vol. 37, No. 1, 2000, pp. 30-36.
    • (2000) Journal of Aircraft , vol.37 , Issue.1 , pp. 30-36
    • Phillips, W.F.1
  • 10
    • 0032631917 scopus 로고    scopus 로고
    • Phugoid approximation revisited
    • Kamesh, S., and Pradeep, S., "Phugoid Approximation Revisited," Journal of Aircraft, Vol. 36, No. 2, 1999, pp. 465-467.
    • (1999) Journal of Aircraft , vol.36 , Issue.2 , pp. 465-467
    • Kamesh, S.1    Pradeep, S.2
  • 11
    • 0032083977 scopus 로고    scopus 로고
    • A century of phugoid approximations
    • Pergamon, Tarrytown, NY
    • Pradeep, S., "A Century of Phugoid Approximations," Aircraft Design, Vol. 1, Pergamon, Tarrytown, NY, 1998, pp. 89-104.
    • (1998) Aircraft Design , vol.1 , pp. 89-104
    • Pradeep, S.1
  • 12
    • 19644388791 scopus 로고    scopus 로고
    • Refined phugoid approximations for conventional aircraft
    • Kamesh, S., and Pradeep, S., "Refined Phugoid Approximations for Conventional Aircraft," AIAA Paper 98-4269, 1998.
    • (1998) AIAA Paper , vol.98 , Issue.4269
    • Kamesh, S.1    Pradeep, S.2
  • 13
    • 0032023095 scopus 로고    scopus 로고
    • Thrust offset effect on longitudinal dynamic stability
    • Bloy, A. W., "Thrust Offset Effect on Longitudinal Dynamic Stability," Journal of Aircraft, Vol. 35, No. 6, 1998, pp. 343-344.
    • (1998) Journal of Aircraft , vol.35 , Issue.6 , pp. 343-344
    • Bloy, A.W.1
  • 16
    • 0003703360 scopus 로고
    • U.S. Government Printing Office, Washington, DC
    • Committee for Extension to the Standard Atmosphere, U. S. Standard Atmosphere, U.S. Government Printing Office, Washington, DC, 1976.
    • (1976) U. S. Standard Atmosphere
  • 17
    • 19644373705 scopus 로고
    • Phugoid characteristics of a YF-12 airplane with variable-geometry inlets obtained in flight tests at a mach number of 2.9
    • Dec.
    • Powers, B.C., "Phugoid Characteristics of a YF-12 Airplane with Variable-Geometry Inlets Obtained in Flight Tests at a Mach Number of 2.9," NASA TP 1107, Dec. 1977.
    • (1977) NASA TP , vol.1107
    • Powers, B.C.1
  • 20
    • 85002965999 scopus 로고
    • Thrust/speed effects on long-term dynamics of aerospace planes
    • Sachs, G., "Thrust/Speed Effects on Long-Term Dynamics of Aerospace Planes," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 1050-1053.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.4 , pp. 1050-1053
    • Sachs, G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.