منابع مشابه
2D Aircraft Trim
The purpose of this document is to discuss a 2-dimensional trim model for an aircraft along with the necessary mathematical methods to solve the problem, the computer implementation of the method and the results. The aircraft is climbing at a constant translational velocity, i.e. the aircraft is not accelerating. The 2-dimensional simplification; restricting the motion of the aircraft to longit...
متن کاملModeling, simulation and analysis of a multi degree of freedom aircraft wing model
This paper presented methods to determine the aerodynamic forces that acton an aircraft wing during flight. These methods are initially proposed for asimplified two degree-of-freedoms airfoil model and then are extensivelyapplied for a multi-degree-of-freedom airfoil system. Different airspeedconditions are considered in establishing such methods. The accuracy of thepresented methods is verifie...
متن کاملDesign and Analysis of Aircraft Wing
In the present study, a general aviation airplane is designed and analyzed. The design process starts with a sketch of how the airplane is envisioned. Weight is estimated based on the sketch and a chosen design mission profile. A more refined method is conducted based on calculated performance parameters to achieve a more accurate weight estimate which is used to acquire the external geometry o...
متن کاملNonlinear Aeroelastic Analysis of Joined-wing Aircraft
Joined-wing aircraft are being designed for ‘sensorcraft’ configuration. Joined wings lead to multiple load paths and constraints. The focus of this work is to understand the nonlinear structural as well as aeroelastic behavior of joined wings. The paper presents a formulation for the nonlinear aeroelastic analysis of joined wings. Results are presented for two joined wings configurations. Over...
متن کاملObliique-Wing Aircraft
The application of the eigensystem synthesis technique to place the closed-loop eigenvalues and shape the closed-loop eigenvectors has not been practical for active flutter suppression, primarily because of the availability of only one control surface (aileron) for flutter suppression. The oblique-wing aircraft, because of its configuration, provides two independent surfaces (left and right ail...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: International Journal of Astronautics and Aeronautical Engineering
سال: 2019
ISSN: 2631-5009
DOI: 10.35840/2631-5009/7530