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Dynamic Stability of Columns under Nonconservative Forces pp 145–153Cite as

Columns under a Rocket-Based Follower Force and with a Lumped Mass

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Part of the book series: Solid Mechanics and Its Applications ((SMIA,volume 255))

Abstract

The experiment described in Chap. 10 demonstrated that the cantilevered column under a rocket thrust lose its stability by flutter. This chapter will take a similar but more quantitative experimental approach to the column subjected to a rocket thrust and equipped with a lumped mass. The stability analysis is carried out by applying the finite element method to discuss the effect of a rigid body on the flutter bound.

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References

  1. Kounadis, A. N., & Katsikadelis, J. T. (1980). On the discontinuity of the flutter load for various types of cantilevers. International Journal of Solid and Structures, 16, 375–383.

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  5. Sugiyama, Y., Matsuike, J., Ryu, B.-J., Katayama, K., Kikoi, S., & Enomoto, N. (1995). Effect of concentrated mass on stability of cantilevers under rocket thrust. AIAA Journal, 33(3), 499–503.

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  6. Katayama, K. (1997). Experimental verification of the effect of rocket thrust on the dynamic stability of cantilevered columns. Doctoral Thesis, Department of Aerospace Engineering, Osaka Prefecture University.

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Authors and Affiliations

  1. Small Spacecraft Systems Research Center, Osaka Prefecture University, Sakai, Osaka, Japan

    Yoshihiko Sugiyama

  2. Department of Mechanical Systems Engineering, Yamagata University, Yonezawa, Japan

    Mikael A. Langthjem

  3. Daicel Corporation, Tatsuno, Hyogo, Japan

    Kazuo Katayama

Authors
  1. Yoshihiko Sugiyama
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  2. Mikael A. Langthjem
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  3. Kazuo Katayama
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Corresponding author

Correspondence to Yoshihiko Sugiyama .

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Sugiyama, Y., Langthjem, M.A., Katayama, K. (2019). Columns under a Rocket-Based Follower Force and with a Lumped Mass. In: Dynamic Stability of Columns under Nonconservative Forces. Solid Mechanics and Its Applications, vol 255. Springer, Cham. https://doi.org/10.1007/978-3-030-00572-6_11

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  • DOI: https://doi.org/10.1007/978-3-030-00572-6_11

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-00571-9

  • Online ISBN: 978-3-030-00572-6

  • eBook Packages: EngineeringEngineering (R0)

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