Record Details

Engine-airframe integration during conceptual design for military application

DSpace at IIT Bombay

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Field Value
 
Title Engine-airframe integration during conceptual design for military application
 
Creator SANGHI, V
KUMAR, SK
SUNDARARAJAN, V
SANE, SK
 
Description Conceptual design has critical leverage on the entire course of design processes because it addresses the issue of selecting the baseline design to optimally accomplish the specified set of requirements. Conceptual-design software has been developed to determine the optimal engine-ail-frame match over a given mission role, its multimission capabilities, and the size and weight of the optimum engine cycle. Its capabilities are demonstrated over three combat mission applications. The results are presented to indicate the optimum designs over these missions, interaction effects of a few design variables, and the future course of developments in propulsion-system technology. The results also include a preliminary estimate of the impact of thrust-vectored takeoff and landing and a variable-capacity, low-pressure turbine on engine-cycle selection and overall aircraft sizing.
 
Publisher AMER INST AERONAUT ASTRONAUT
 
Date 2011-07-15T08:54:47Z
2011-12-26T12:49:22Z
2011-12-27T05:39:15Z
2011-07-15T08:54:47Z
2011-12-26T12:49:22Z
2011-12-27T05:39:15Z
1998
 
Type Article
 
Identifier JOURNAL OF AIRCRAFT, 35(3), 380-386
0021-8669
http://dx.doi.org/10.2514/2.2335
http://dspace.library.iitb.ac.in/xmlui/handle/10054/4210
http://hdl.handle.net/10054/4210
 
Language en