Email this article Dynamic behavior of wing leading edge assembly with thermal protection coating
- Authors: Antuf’ev B.A.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 60, No 1 (2017)
- Pages: 9-12
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229963
- DOI: https://doi.org/10.3103/S1068799817010020
- ID: 229963
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Abstract
The paper presents an approximate solution of a problem on dynamic behavior of a wing leading edge assembly discretely reinforced by a system of ribs and coated with thermal protection coating.
About the authors
B. A. Antuf’ev
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: antufjev.bor@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
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