Lift force for cylindrical and elliptical coandă aircraft design

Small aerial vehicles possess advantages in terms of size and accessibility in performing a variety of tasks. Presently, their design and performance is dependent on variations of conventional aerodynamic configurations (fixed- and rotary-wing). A disadvantage for these configurations is the aerodyn...

Full description

Saved in:
Bibliographic Details
Main Authors: Abdul Hamid, Mohd Faisal, Mohd Rafie, Azmin Shakrine, Gires, Ezanee, Abu Talib, Abd. Rahim
Format: Article
Language:English
Published: Science Publishing Corporation 2018
Online Access:http://psasir.upm.edu.my/id/eprint/74838/1/Lift%20force.pdf
http://psasir.upm.edu.my/id/eprint/74838/
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Universiti Putra Malaysia
Language: English