A Method of Calculating the Small-Sized Combustion Chambers

A model of structural-geometric dimension calculation and integral characteristic estimation of the combustion chambers of the small-sized gas turbine engines at their conceptual design stage are developed.

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Bibliographische Detailangaben
Veröffentlicht in:	Russian aeronautics 2019-07, Vol.62 (3), p.469-475
Hauptverfasser:	Lanskii, A. M., Lukachev, S. V., Matveev, S. G., Kolomzarov, O. V.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft and Rocket Engine Design and Development Automotive Engineering Combustion chambers Engineering Gas turbine engines Repair & maintenance
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	A model of structural-geometric dimension calculation and integral characteristic estimation of the combustion chambers of the small-sized gas turbine engines at their conceptual design stage are developed.
ISSN:	1068-7998 1934-7901
DOI:	10.3103/S1068799819030152