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...
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 |
Similar Items
-
Coanda configured aircraft: a preliminary analytical assessment
by: Abdul Hamid, Mohd Faisal, et al.
Published: (2017) -
First principle analysis of Coandă Micro Air Vehicle aerodynamic forces for preliminary sizing
by: Djojodihardjo, Harijono, et al.
Published: (2017) -
Aerodynamics and flight mechanics of MAV based on Coanda effect
by: Ahmed, R. I., et al.
Published: (2017) -
Review on progress and application of active flow control devices - Coandă effect on unmanned aerial vehicles
by: Ahmed, Riyadh Ibraheem, et al.
Published: (2017) -
Circulation control aircraft design: assessment on the channel-wing lift-thrust performance characteristics
by: Md Shafie, Muhammad Alimin, et al.
Published: (2019)