Modelling Combined Heat Exchange in the Leading Edge of Perspective Aircraft Wing
Bauman Moscow State Technical University, Moscow, Russian Federation
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In this paper gas dynamic numerical modelling of leading edge flow is presented and thermal loading parameters are determined. Numerical modelling of combined radiative and conductive heat transfer of the wing edge is carried out, thermal state of structure is given and the results are analyzed.
© Owned by the authors, published by EDP Sciences, 2015
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