Determination of operating point for a propulsive wing UAV using CFD

This report seeks to determine the operating point of a 2D propulsive wing UAV using CFD. CFD simulations were performed using a 2D RANS k-ε turbulence model and the rotating flow was captured using the moving reference frame method. Lift and drag were obtained for different angle of attacks via a c...

Full description

Saved in:
Bibliographic Details
Main Author: Chan, Chee Shuan
Other Authors: Basman Elhadidi
Format: Final Year Project
Language:English
Published: 2018
Subjects:
Online Access:http://hdl.handle.net/10356/74857
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