What is it about?
This paper presents a Pareto approach for bi-objective optimization to design for optimal performance of turboprop engines matching power requirements of a propeller-driven aircraft.
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Why is it important?
The conflicting objectives that have been considered are the power specific fuel consumption and the specific power.
Perspectives
the present methodology is rapid to optimize turboprops in the preliminary design phases, or identify candidate engines matching with given aircraft performance.
PHD ADEL GHENAIET
Laboratory of Energy Conversion Systems, Faculty of Mechanical Engineering and Process Engineering, University of Science and Technology, Houari Boumediene, BP 32 El-Alia, Bab-Ezzouar, 16111, Algiers, Algeria
Read the Original
This page is a summary of: Optimum Design of Turboprop Engines Using Genetic Algorithm, Journal of Propulsion and Power, November 2009, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.38817.
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