A mathematical model of heat shielding for a nose cone taking into account critical flight situations

A mathematical model of heat shielding for a nose cone taking into account critical flight situations

A mathematical model of heat shielding for a nose cone is constructed taking into account the in-flight change of states and critical situations. The situations are estimated by the specific factors.

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Bibliographische Detailangaben
Veröffentlicht in:Russian aeronautics 2014, Vol.57 (1), p.100-106
Hauptverfasser: Urazbakhtin, F. A., Kharinova, Yu. Yu, Urazbakhtin, V. F.
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft and Rocket Engine Theory
Automotive Engineering
Construction
Engineering
Heat shielding
Mathematical models
Nose cones
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Beschreibung
Zusammenfassung:A mathematical model of heat shielding for a nose cone is constructed taking into account the in-flight change of states and critical situations. The situations are estimated by the specific factors.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799814010140