Case Study on Avoiding Stalling Effect Due to Failure of Flaps While Flying in Storm

 




 

Kok, Yin Hoo (2011) Case Study on Avoiding Stalling Effect Due to Failure of Flaps While Flying in Storm. Final Year Project (Other), Tunku Abdul Rahman University College.

[img] Text
KokYinHooFT.zip
Restricted to Registered users only

Download (1MB)

Abstract

An airplane can be made to stall in any pitch attitude or angle of attack or at any airspeed but is commonly practiced by reducing the speed to the not accelerated stall speed, at a safe altitude. The main objective of this dissertation is to ensure the aircraft is flying at the safe level and prevent stalling effect while flying in the storm condition with the function of flaps. Different conventional aircraft with the type of flaps will be discussed in this project. The effect of coefficient of lift and drag force will be shown. The computation is the nature of this research. C-H- programming software will be applied to compute final result which is the flap angle.

Item Type: Final Year Project
Subjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. Astronautics
Faculties: School of Technology > Advance Diploma in Technology (Mechanical and Manufacturing Engineering)
Depositing User: Library Staff
Date Deposited: 25 Sep 2019 01:14
Last Modified: 25 Sep 2019 07:01
URI: https://eprints.tarc.edu.my/id/eprint/8936