Aerodynamic measurements of an airfoil with a spoiler

A rapidly deployed spoiler on the upper surface of a wing induces adverse lift and moment during aircraft landing. These adverse effects are associated with the strong starting vortex, which is caused by the shear flow at the spoiler tip and is located downstream of the deflected spoiler. This thesi...

Full description

Saved in:
Bibliographic Details
Main Author: Gu, Weidong.
Other Authors: Yeung, William Wai Hung
Format: Theses and Dissertations
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/19937
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English
Be the first to leave a comment!
You must be logged in first