DESIGN OF PROCESS OF THERMAL NON-DESTRUCTIVE CONTROL NON-METAL MULTI-LAYERED ELEMENTS OF GLIDER OF AIR SHIP
Abstract
Now days the questions related to the thermal non-destructive control of aviation constructions are more vital. In the article a mathematical design and model design of process of thermal control are considered for the exposure of removing layer by layer of filler from edging of multi-layered construction of air ship. Influence of temperature and duration of heating is considered on realization of thermal non-destructive control.
About the Authors
N. P. Zaets
ВУНЦ ВВС «ВВА им. проф. Н.Е. Жуковского и Ю.А. Гагарина»
Russian Federation
Russian Federation
O. N. Karpenko
ВУНЦ ВВС «ВВА им. проф. Н.Е. Жуковского и Ю.А. Гагарина»
Russian Federation
Russian Federation
V. S. Oleshko
Военный институт МАИ (НИУ)
Russian Federation
Russian Federation
I. A. Chizhov
ВУНЦ ВВС «ВВА им. проф. Н.Е. Жуковского и Ю.А. Гагарина»
Russian Federation
Russian Federation
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Review
For citations:
Zaets N.P., Karpenko O.N., Oleshko V.S., Chizhov I.A. DESIGN OF PROCESS OF THERMAL NON-DESTRUCTIVE CONTROL NON-METAL MULTI-LAYERED ELEMENTS OF GLIDER OF AIR SHIP. Civil Aviation High Technologies. 2016;(225):55-63. (In Russ.)
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