Analysis and Optimization of Incompressible Inviscid Flow around Split Flap Airfoils

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Analysis and Optimization of Incompressible Inviscid Flow around Split Flap Airfoils

Generally airfoils are designed for cruise flight conditions; but during take-off and landing, when the airplane flies at low speeds and small angles of attacks, the lift provided by single airfoils is not sufficient, and an extra lift is required for safe landing and take-off. In this condition...

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Bibliographic Details
Main Author:	Mohamed Ahmed, Osman
Format:	Thesis
Language:	English English
Published:	1997
Subjects:	Flaps (Airplanes) - Aerofoils - Analysis - Case studies
Online Access:	http://psasir.upm.edu.my/id/eprint/10007/ http://psasir.upm.edu.my/id/eprint/10007/1/FK_1997_8_A.pdf

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