Lift and Drag of Non-conventional Wings at Subsonic Speeds and Zero Angle of Attack - An Experimental Investigation
Various non-conventional wing development shows potential in increasing the aerodynamic performance of airplanes. If the non-conventional wing only improves the aerodynamic performance by a small margin, conventional wing is still a better option for airline operators. This provides opportunity to c...
Main Authors: | Al-Obaidi Abdulkareem Shafiq Mahdi, Wei Ting Chern |
---|---|
Format: | Article |
Language: | English |
Published: |
EDP Sciences
2018-01-01
|
Series: | MATEC Web of Conferences |
Online Access: | https://doi.org/10.1051/matecconf/201815202017 |
Similar Items
-
Investigation of a NACA0012 Finite Wing Aerodynamics at Low Reynold’s Numbers and 0º to 90º Angle of Attack
by: Shahrooz Eftekhari, et al.
Published: (2019-03-01) -
IMPLEMENTATION OF SEMI-EMPIRICAL MODELS TO ENHANCE THE ACCURACY OF PANEL METHODS FOR DRAG PREDICTION AT SUPERSONIC SPEEDS
by: Abdulkareem Shafiq Mahdi Al-Obaidi
Published: (2011-12-01) -
Supersonic interference pressure drag between wing and body at zero lift /
by: Peline, Julius P.
Published: (1958) -
Effect of vortex generator on the flow field over a conventional delta wing in subsonic flow condition at higher angles of attack
by: Patil Manthan, et al.
Published: (2021-01-01) -
The lift of thin airfoils at high-subsonic speeds
by: Willmarth, William W.
Published: (1954)