Optimal Landing Ground_run for FAR_23 Aircraft

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Hosseinian Nasab, Amir | 2016

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Type of Document: M.Sc. Thesis
Language: Farsi
Document No: 48510 (45)
University: Sharif University of Technology
Department: Aerospace Engineering
Advisor(s): Malaek, Mohammad Bagher
Abstract:
As demand for floght has been incrased, a critical questin to pose is that is it economic to use larger Ailplanes or smaller Airplanes with higher flight frequency should be use. It is self evident that in a large Airplane the whole seats can not be accupied in all cases. Conversly, in small Airplanes, in most cases the seats are accupied but for aqual demand there most be more flights.In order to increase the number of flights, new methods should be used in such a way that smaller Airplanes live the Runway as soon as possible.In this project with modelling all effective factor regarding to Landing of a commercial FAR_23 Airplane, the Landing distance and thr erquired time for living the Runway(in presence of effective fators) will be considered.This factors including :
1. Configuration Control factors such as Flap and Spoiler
2. Factors regarding to propulsion system and reverse
3. Mechanical Factors such as Braking and Tires
4. Environmental factors like Runway material
Keywords:
Thrust Reversal ; Landing Process ; Optimal Control ; Landing Run ; Landing Time Optimization

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