Autor: |
Rotaru, Constantin, Cîrciu, Ionică, Edu, Raluca Ioana, Ciuică, Oliver, Mihai, Eduard |
Předmět: |
|
Zdroj: |
Proceedings of the Scientific Conference AFASES; May2015, Vol. 2, p475-480, 6p |
Abstrakt: |
This paper presents an analytical evaluation of the airplane yawing moment, based on the general theory of the aerodynamic design, with details leading first to the separate formulation of the Fourier coefficients in the series solution to the Prandtl's lifting-line theory, followed by the numerical calculation of the sidewash gradient of the vertical tail for a standard configuration of an airplane geometry. Several approaches of the vortex strength and vortex span factors were considered to choose the methodology that better predicts the airplane dynamic handling quality requirements. [ABSTRACT FROM AUTHOR] |
Databáze: |
Complementary Index |
Externí odkaz: |
|