Author Details

Крупенич, И. Н.

Issue	Section	Title	File
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	Automated system of gas turbine engines termogazdynamic calculation and analysis	(Rus)
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	The method of bypass engines turbocompressors structural-geometric parameters matching	(Rus)
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	Automated variant aircraft GTE turbocompressor flow path designing	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Investigation of relative geometric parameters influence on bypass engine mass	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Problem formulation of bypass engine parameters optimization with a preselected gas generator	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»	(Rus)
Vol 11, No 3-3 (2012): Special Issue	CONFERENCE MATERIALS	Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system	(Rus)
Vol 13, No 5-3 (2014): Special Issue	ISSUE WITHOUT SECTION	Computer-aided system of virtual gas turbine engine testing	(Rus)
Vol 10, No 3-3 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Dataware of virtual lab for gas turbine engine testing	(Rus)
Vol 10, No 3-4 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium	(Rus)

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