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.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsReferences
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.
Park, Y. P., & Mote, C. D., Jr. (1985). The maximum controlled follower force on a free-free beam carrying a concentrated mass. Journal of Sound and Vibration, 98, 247–256.
Barsoum, R. S. (1971). Finite element method applied to the problem of stability of a nonconservative systems. International Journal for Numerical Methods in Engineering, 3(1), 63–87.
Sugiyama, Y., Matsuike, J., Ryu, B.-J., Katayama, K., Kinoi, S., & Enomoto, H. (1994). Flutter of cantilevered columns subjected to a rocket end thrust and having an intermediate concentrated mass. In AIAA-94-1622, AIAA/ASME/ASCE/AHS/ASC 35th Structures, Structural Dynamics, and Materials Conference (Hilton Head) (pp. 2419–2427).
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.
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.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2019 Springer Nature Switzerland AG
About this chapter
Cite this chapter
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
Download citation
DOI: https://doi.org/10.1007/978-3-030-00572-6_11
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-00571-9
Online ISBN: 978-3-030-00572-6
eBook Packages: EngineeringEngineering (R0)