Structural finite-element modeling strategies for conformal load-bearing antenna structure (CLAS) (Air Force contract F33615-C-93-3200)

Allen J. Lockyer; Kevin H. Alt; Jayanth N. Kudva; Robert W. Kinslow; Allan C. Goetz

doi:10.1117/12.276604

19 June 1997 Structural finite-element modeling strategies for conformal load-bearing antenna structure (CLAS) (Air Force contract F33615-C-93-3200)

Allen J. Lockyer, Kevin H. Alt, Jayanth N. Kudva, Robert W. Kinslow, Allan C. Goetz

Author Affiliations +

Proceedings Volume 3046, Smart Structures and Materials 1997: Smart Electronics and MEMS; (1997) https://doi.org/10.1117/12.276604
Event: Smart Structures and Materials '97, 1997, San Diego, CA, United States

Abstract

As the Wright Lab Air Force military contrast `Smart Skin Structures Technology Demonstration' (S³TD) Contract No. F33615-C-93-3200 draws toward conclusion, pertinent features of the program finite element modeling are presented. Analysis was performed to predict the structural performance of a complex multilayered composite panel that will be tested structurally (and electrically) for the final program deliverable. Application of finite element modeling to predict component load path and strain distribution in sandwich panel construction has been reported elsewhere in the literature for more standard applications. However, the unauthordox sandwich configuration lay-up posed by the quite revolutionary S³TD CLAS aircraft fuselage panel demonstration article merits further discussion. Difficulties with material selection, the stumbling block for many programs, are further exacerbated by conflicting material properties required to support simultaneous electrical and structural performance roles. The structural analysis challenge derives from S³TD's unique program goal, namely, to investigate load bearing antennas structural configurations, rather than conventional structurally inefficient `bolt in' installations, that have been the modus operandi for tactical aircraft antenna installations to date. Discussed below is a cost saving strategy where use of linear finite element analysis has been employed in the prediction of key structural parameters, and validated with risk reduction sub panel measurements, before proceeding to the final fabrication of a full scale 36 by 36 inch CLAS panel demonstration article.

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Allen J. Lockyer, Kevin H. Alt, Jayanth N. Kudva, Robert W. Kinslow, and Allan C. Goetz "Structural finite-element modeling strategies for conformal load-bearing antenna structure (CLAS) (Air Force contract F33615-C-93-3200)", Proc. SPIE 3046, Smart Structures and Materials 1997: Smart Electronics and MEMS, (19 June 1997); https://doi.org/10.1117/12.276604

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