Numerical Computation of Subsonic Oscillatory Airforce Coefficients for Wing-Winglet Configurations
This paper presents the theoretical development and numerical results of a lifting-surface theory for calculating oscillating airforce coefficients for wing-winglet configurations and it follows the author's previous paper on the extension of Davies' T-tail theory for cruciform-tail config...
Main Author: | |
---|---|
Format: | Article |
Language: | English |
Published: |
SAGE Publishing
2007-10-01
|
Series: | Journal of Algorithms & Computational Technology |
Online Access: | https://doi.org/10.1260/174830107782424093 |