Abstract
The theory and application of the prescribed averaged temperatures (PAT) is presented. The PAT provides a very systematic way to depict temperatures obtained from thermal analyzers on to structural finite element models. The PAT fills the gap between the thermal and structural analyses.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
25.4 Literature
Appel, S., 1996, Interpolation of Lumped Parameter Temperatures for Thermo-elastic FEM Analysis with SINAS, Proceedings Conference on Spacecraft Structures &Mechanical Testing, ESA SP-386, pages 277–281.
Bathe, K.J., 1986, Finite Element Methods, Springer-Verlag, 1986.
Cook, D., Malkus, D.S., Plesha, M.E., 1989, Concepts and Applications of Finite Element Analysis, third edition, John Wiley & Sons, ISBN0-471-84788-7.
Thorton, E.A, 1996, Thermal Structures for Aerospace Application, ISBN 1-56347-6, AIAA Education Series.
Tsai, J.R., 2004, Overview of Satellite Thermal Model, Journal of Spacecraft & Rockets, Vol 41, No. 1, pages 120–125.
Rights and permissions
Copyright information
© 2008 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
(2008). Prescribed Averaged Temperatures. In: Spacecraft Structures. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-75553-1_25
Download citation
DOI: https://doi.org/10.1007/978-3-540-75553-1_25
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-75552-4
Online ISBN: 978-3-540-75553-1
eBook Packages: EngineeringEngineering (R0)