The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties

The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties

The equations of the mathematical model are solved in terms of special functions. The results for the design scheme of the aircraft forebody are obtained with a guaranteed accuracy by the stable method of functional normalization.

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Veröffentlicht in:Russian aeronautics 2018-04, Vol.61 (2), p.156-164
Hauptverfasser: Bakulin, V. N., Vinogradov, Yu. I., Men’kov, G. B
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft design
Automotive Engineering
Conical shells
Engineering
Protective coatings
Structural Mechanics and Strength of Flight Vehicles
Temperature dependence
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Beschreibung
Zusammenfassung:The equations of the mathematical model are solved in terms of special functions. The results for the design scheme of the aircraft forebody are obtained with a guaranteed accuracy by the stable method of functional normalization.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799818020022