The Design of Impact Resistance of Missile Recorder Protective Shell

Xi Hong Ma; Chang Long Li; Jun Liu; Tao Sun

doi:10.4028/www.scientific.net/AMR.503-504.884

Paper Titles

Design a Two-Harmonics Transmission Mechanism with Roller Chain
p.867

Optimal Design of a Vehicular Charged-Air Cooler Based on Numerical Simulation of Thermal-Hydraulic Performances
p.872

The Finite Element Analysis of Rotor Contact Strength for a High-Speed Traction Motor
p.876

Comparative Analysis of Parabolic and Hyperbolic Flexure Hinges Using Closed-Form Equations
p.880

The Design of Impact Resistance of Missile Recorder Protective Shell
p.884

Role of Ion Transport in the Actuation of Cellulose Based EAPap
p.888

Multi-Jack Single-Drive Semi-Flexible Nozzle Mechanism Design and Simulation
p.892

Study of the Loading Arms of the Side-Crane Used for Container
p.896

Force Model and Simulation Analysis about Two-Ring Speed Reducer
p.900

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 503-504The Design of Impact Resistance of Missile...

The Design of Impact Resistance of Missile Recorder Protective Shell

Abstract:

The instability of the testing equipment protective shell is one of the importance issues in the design of testing equipment. In order to analyze the protective shell to external shocks instability problem, the shell instability of empirical formula was used to calculate the critical buckling load and the linear buckling was analysed to compare the simulation results with theoretical values and the error in control range by using finite element method.The calculations show that the finite element method for buckling analysis to provide guidance for the design is feasible.

You might also be interested in these eBooks

Frontiers of Manufacturing Science and Measuring Technology II

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 503-504)

Pages:

884-887

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.503-504.884

Citation:

Cite this paper

Online since:

April 2012

Authors:

Xi Hong Ma, Chang Long Li, Jun Liu, Tao Sun

Keywords:

Buckling, Finite Element (FE) Simulation, Protective Shell

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Bruce Kaufman. A nonvolatile solid-state Recorder for 100, 000g. Enviroments[J]. sensors Magazine. Vol. 17, NO6, June 2000, 46-51.

Google Scholar

[2] Nicholas F. Morris. Shell stability: the long road from theory to practice. Original Research Article. Engineering Structures, Volume 18, Issue 10, October 1996, Pages 801-806.

DOI: 10.1016/0141-0296(96)00009-0

Google Scholar

[3] Bruce Kaufman. This solid-state Recorder Rides in a Bullet. Sensors Magazine. Vol. 7, NO. 3, March 2005, 4-5.

Google Scholar

[4] Budiansky,B., Roth R.S., Axisymmetric dynamic buckling of clamped shallow spherical shells,J. Math, phys., 1954, 32: 276-239.

Google Scholar

[5] C. Hühne,R. Rolfes, E. Breitbach, J. Temer. Robust design of composite cylindrical shells under axial compression-Simulation and validation Original Research Article. Thin-Walled Structures, Volume 46, Issues 7-9, July-September 2008, Pages 947-962.

DOI: 10.1016/j.tws.2008.01.043

Google Scholar

[6] Marios K Chryssanthopoulos, Carlo Poggi, Andrea Spagnoli. Buckling design of conical shells based on validated numerical models Original Research Article. Thin-Walled Structures, Volume 31, Issues 1-3, May 1998, Pages 257-270.

DOI: 10.1016/s0263-8231(98)00006-8

Google Scholar

[7] H. Mahfuz Z.Y. Hui Zhu,A. Haque,A. Abutalib, etc. Investigation of high-velocity impact on integral armor using finite element method. International Journal of Impact Engineering. 24, 203-217, (2000).

DOI: 10.1016/s0734-743x(99)00047-0

Google Scholar