Adaptive winglet
Journal Title: Механіка гіроскопічних систем - Year 2018, Vol 0, Issue 35
Abstract
Winglet are intended to improve the efficiency of fixed-wing aircraft by reducing inductive drag. Such devices increase the effective aspect ratio of a wing without materially increasing the wingspan. Winglets provide fuel efficiency of 3.5-4.5% at cruising speed. For airplanes that often change the flight mode, the winglets are less effective. In order to increase the effectiveness of winglets on all modes of flight, the concept of adaptive winglets is developed. The concept of a winglet with the possibility of turning around the vertical axis of the aircraft. The adaptive winglets are designed to set the optimal angle of attack for the winglets on all flight modes of the aircraft, as well as to control the aircraft in the yaw and roll channel. The possibility of turning the winglets allows you to control the distribution of the lift force in the end part of the wing.
Authors and Affiliations
Т. О. Semkiv,, D. М. Zinchenko
VIBRATIONS OF AIRCRAFT ENGINES TURBINE BLADES WITH HYSTERETIC ENERGY DISSIPATION
<p class="MsoNormal" style="tab-stops: 117.85pt;"><span style="font-size: 14.0pt; line-height: 115%; font-family: 'Times New Roman','serif'; mso-ansi-language: UK;" lang="UK">Vibrations</span><span style="font-size: 14.0...
Визначення пріоритетів ризикових ситуацій при керуванні динамічними системами
The paper considers the actual problem of prioritization the risk situations during controlling process of the dynamic systems of different nature. Studied that current tools for solving the problem are quite limited and...
Estimation of state of flight simulator motion system
Solution of problem of status analyzing of motion systems, deficiency identification of both motion systems and their hydraulic actuators, and suitability assessment of motion systems for use in aircraft flight simulator...
ЗМЕНШЕННЯ ОПОРУ ТЕРТЯ ЛІТАКА ШЛЯХОМ МІКРОВИДУВУ ЧЕРЕЗ ПРОНИКНІ ДІЛЯНКИ ПОВЕРХНІ КРИЛА
<strong><strong></strong></strong>На прикладі крила літака Ан-124 було досліджено переваги та особливості впливу на опір літака мікровидуву повітря через пористу ділянку обтічної поверхні. Проведено параметричний аналіз...
EXPERIMENTAL TESTS OF AN ALGORITHM OF ROLL AND PITCH ESTIMATION USING ONLY OPTICAL INFORMATION
The research concerns the problem of carrying out experimental tests of an image-based measurement system that is able to detect horizon line and calculate it relative position on the image in terms of roll and pitch ang...