Record Details

Digital simulation of propulsion system performance for cycle optimization studies

DSpace at IIT Bombay

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Field Value
 
Title Digital simulation of propulsion system performance for cycle optimization studies
 
Creator SANGHI, V
SANE, SK
 
Subject prediction
 
Description The propulsion system has a high cost of ownership, long development period, and bears a dominant influence on aircraft mission performance. Thus identification of an optimum engine cycle right in the conceptual design, which makes the aircraft most responsive in terms of the cost as well as performance, to the specified baseline mission is the prime necessity. Engine steady-state performance estimates form an important input to cycle optimization studies. This paper defines the conceptual design constraints, and extends the methods reported in open literature to describes a mathematical model for steady-state performance prediction of two- and three-spool military engines. The proposed formulation is robust, computationally fast, consistent with conceptual design accuracy, and is readily adaptable for integration into a parametric conceptual design software.
 
Publisher FREUND PUBLISHING HOUSE LTD
 
Date 2011-07-29T20:22:47Z
2011-12-26T12:52:37Z
2011-12-27T05:39:04Z
2011-07-29T20:22:47Z
2011-12-26T12:52:37Z
2011-12-27T05:39:04Z
1999
 
Type Article
 
Identifier INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 16(1), 27-37
0334-0082
http://dspace.library.iitb.ac.in/xmlui/handle/10054/7820
http://hdl.handle.net/10054/7820
 
Language en