Air-breathing propulsion engines play an important role in the development of both civil and military aircraft Design optimization of such engines can lead to higher power, or more thrust for less fuel consumption. A multimission propulsion engine design can be modeled mathematically as a multivariable global optimization problem, with a sequence of subproblems, which are specific to the mission events defined through Mach number, altitude, and power setting combinations.
Optimization of Air-Breathing Propulsion Engine Concepts
1997-04-01
Conference paper
No indication
English
Cascade Optimization Strategy for Aircraft and Air-Breathing Propulsion System Concepts
Online Contents | 1997
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