Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/8975
Title: Aerospace structure design using structural response of a payload carried by jet fighter
Authors: Kaplan, Engin Metin
Acar, Erdem
Ozer, Mehmet Bulent
Keywords: Structural Optimization
Store Vibration
Structural Response
MIL-STD-810
Military Specification
Vibration
Issue Date: 2022
Publisher: Gazi Univ, Fac Engineering Architecture
Abstract: Purpose: The aim of this study is to evaluate the structural responses proposed by military specifications with real test conditions and also compare the effects of usage ANN predicted and military specification loads in design of aerospace structures. Theory and Methods: Vibration responses in structural design is used as PSD in the frequency domain. Loads for structural design purposes are calculated with random loads using PSD data between 20-300 Hz frequency bands. Results: An aerospace structure is designed according to the ANN predictions, military specification proposal and experimental design loads. Supports designed based on experimental and predicted loads are lighter than the support designed according to the military specification load. Conclusion: It was observed that military specification loads exhibit conservatism. This conservatism makes the aerospace structures complex and heavier. Also, more engineering effort and production cost is occurred since the loads are high with respect to real environmental conditions.
URI: https://doi.org/10.17341/gazimmfd.898550
https://search.trdizin.gov.tr/yayin/detay/508611
https://hdl.handle.net/20.500.11851/8975
ISSN: 1300-1884
1304-4915
Appears in Collections:Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
TR Dizin İndeksli Yayınlar / TR Dizin Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection

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