Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles-Reference-Cited by-同舟云学术

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Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles

Published:2017-07 Issue: Volume:136 Page:312-331
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Persova Marina G.,Soloveichik Yury G.,Belov Vasiliy K.,Kiselev Dmitry S.,Vagin Denis V.,Domnikov Petr A.,Patrushev Ilya I.,Kurskiy Denis N.

Funder

Ministry of Education and Science of the Russian Federation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Heat transfer in a multi-layered thermal protection system under aerodynamic heating;Ferraiuolo;Int. J. Therm. Sci.,2012

2. W.F. Braga, M.B.H. Mantelli, J.L.F. Azevedo, A new approach for the heat balance integral method applied to heat conduction problems, in: Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 2005, pp. 3127–3138.

3. Analytical solution to transient heat conduction in polar coordinates with multiple layers in radial direction;Singh;Int. J. Therm. Sci.,2008

4. Study of the analytical solution to the heat transfer problem and surface temperature in a semi-infinite body with a constant heat flux at the surface and an initial temperature distribution;Zhuang;Heat Mass Transf.,1995

5. Development and flight qualification of the C–SiC thermal protection systems for the IXV;Buffenoir;Acta Astronaut.,2016

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