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Volumn 225, Issue 4, 1999, Pages 779-782

Realistic follower forces

Author keywords

[No Author keywords available]

Indexed keywords


EID: 0000095244     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1998.2290     Document Type: Editorial
Times cited : (71)

References (21)
  • 1
    • 0347959045 scopus 로고
    • Die knicklast des einseitig eingespannten, tangential gedrückten stabes
    • M. BECK 1952 ZAMM 3, 225-228. Die Knicklast des einseitig eingespannten, tangential gedrückten Stabes.
    • (1952) ZAMM , vol.3 , pp. 225-228
    • Beck, M.1
  • 4
    • 85007670840 scopus 로고
    • Dynamic stability of a flexible missile under the constant and pulsating thrust
    • T. R. BEAL 1965 AIAA Journal 3, 486-494. Dynamic stability of a flexible missile under the constant and pulsating thrust.
    • (1965) AIAA Journal , vol.3 , pp. 486-494
    • Beal, T.R.1
  • 5
    • 0039521617 scopus 로고    scopus 로고
    • Stability of a jointed free-free beam under end rocket thrust
    • K. A. MLADENOV and Y. SUGIYAMA 1997 Journal of Sound and Vibration 199, 1-15. Stability of a jointed free-free beam under end rocket thrust.
    • (1997) Journal of Sound and Vibration , vol.199 , pp. 1-15
    • Mladenov, K.A.1    Sugiyama, Y.2
  • 7
    • 0016934965 scopus 로고
    • On an unduly simplified model in the non-conservative problem of elastic stability
    • Y. SUGIYAMA, K. KASHIMA and H. KAWAGOE 1976 Journal of Sound and Vibration 45, 237-247. On an unduly simplified model in the non-conservative problem of elastic stability.
    • (1976) Journal of Sound and Vibration , vol.45 , pp. 237-247
    • Sugiyama, Y.1    Kashima, K.2    Kawagoe, H.3
  • 10
    • 0040113304 scopus 로고
    • Surveys of the experimental studies of instability of the elastic systems subjected to nonconservative forces
    • Y. SUGIYAMA and T. SEKIYA 1971 Journal of the Japan Society for Aeronautical and Space Sciences 19, 61-68. Surveys of the experimental studies of instability of the elastic systems subjected to nonconservative forces (in Japanese).
    • (1971) Journal of the Japan Society for Aeronautical and Space Sciences , vol.19 , pp. 61-68
    • Sugiyama, Y.1    Sekiya, T.2
  • 13
    • 0029272532 scopus 로고    scopus 로고
    • Effect of concentrated mass on stability of cantilevers under rocket thrust
    • Y. SUGIYAMA, J. MATSUIKE B.-J. RYU, K. KATAYAMA, S. KINOI and N. ENOMOTO 1995 AIAA Journal 33, 499-503, 1996 AIAA Journal 34, 212. Effect of concentrated mass on stability of cantilevers under rocket thrust.
    • (1996) AIAA Journal , vol.34 , pp. 212
  • 14
    • 84907177896 scopus 로고    scopus 로고
    • Experimental verification of dynamic stability of vertical cantilevered columns subjected to a sub-tangential force
    • submitted
    • Y. SUGIYAMA, K. KATAYAMA, K. KIRIYAMA and B.-J. RYU Journal of Sound and Vibration. Experimental verification of dynamic stability of vertical cantilevered columns subjected to a sub-tangential force (submitted).
    • Journal of Sound and Vibration
    • Sugiyama, Y.1    Katayama, K.2    Kiriyama, K.3    Ryu, B.-J.4
  • 15
    • 0032163591 scopus 로고    scopus 로고
    • Dynamic stability of Timoshenko columns subjected to subtangential forces
    • B.-J. RYU, K. KATAYAMA and Y. SUGIYAMA 1998 Computers and Structures 68, 499-512. Dynamic stability of Timoshenko columns subjected to subtangential forces.
    • (1998) Computers and Structures , vol.68 , pp. 499-512
    • Ryu, B.-J.1    Katayama, K.2    Sugiyama, Y.3
  • 16
    • 0028531242 scopus 로고
    • On the design of Beck's column
    • U. T. RINGERZT 1994 Structural Optimization 8, 120-124. On the design of Beck's column.
    • (1994) Structural Optimization , vol.8 , pp. 120-124
    • Ringerzt, U.T.1
  • 17
    • 84907177895 scopus 로고    scopus 로고
    • Optimum shape design against flutter of a cantilevered column with an end-mass of finite size subjected to a nonconservative load
    • accepted
    • M. A. LANGTHJEM and Y. SUGIYAMA, Journal of Sound and Vibration. Optimum shape design against flutter of a cantilevered column with an end-mass of finite size subjected to a nonconservative load (accepted).
    • Journal of Sound and Vibration
    • Langthjem, M.A.1    Sugiyama, Y.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.