A method for wrinkling analysis of creased space film under thermal environment
Author:
Funder
the National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s00707-024-03962-7.pdf
Reference44 articles.
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2. Fu, B., Farouki, R.T., Eke, F.O.: Equilibrium configuration of a bounded inextensible membrane subject to solar radiation pressure. Aerosp. Sci. Technol. 68, 552–560 (2017). https://doi.org/10.1016/j.ast.2017.06.018
3. Lu, G.-Y., Zhou, J.-Y., Cai, G.-P., Fang, G.-Q., Lv, L.-L., Peng, F.-J.: Studies of thermal deformation and shape control of a space planar phased array antenna. Aerosp. Sci. Technol. 93, 105311 (2019). https://doi.org/10.1016/j.ast.2019.105311
4. Woo, K., Nandukar, K., Jenkins, C.H.: Effective modulus of creased thin membranes. J. Spacecr. Rocket. 45(1), 19–26 (2008). https://doi.org/10.2514/1.29282
5. Woo, K., Jenkins, C.H.: Analysis of crease-wrinkle interaction for thin sheets. J. Mech. Sci. Technol. 26(3), 905–916 (2012). https://doi.org/10.1007/s12206-011-1247-5
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