Vertical stabilizer - Wikipedia
网页Control surfaces at the tail of a conventional aircraft. The vertical tail of an aircraft typically consists of a fixed vertical stabilizer or fin on which a movable rudder is mounted. A trim tab may similarly be mounted on the rudder.
Aircraft Horizontal and Vertical Tail Design - AeroToolbox
网页2022年9月28日 · The tail assembly (horizontal and vertical stabilizer) is also known as the empennage which originates from the French term empenner which means to “feather an arrow”. Similar to how the feathers on an arrow stabilize the arrow in flight, the tail ensures that the aircraft remains stable through all phases of operation.
Types of Aircraft Tail Structures: Conventional, T-Tail, V-Tail, and ...
网页2024年2月21日 · Vertical stabilizer: This stabilizer is a vertical surface at the tail end of the aircraft, providing stability in the yaw axis (side-to-side movement). The vertical stabilizer helps prevent the aircraft from turning too much to the left or right, ensuring a straight and stable flight path.
垂直尾翼 - 百度百科
网页垂直安定面是垂直尾翼中的固定翼面部分。. 当飞机沿直线作近似匀速直线运动飞行时,垂直安定面不会对飞机产生额外的力矩,但当飞机受到气流的扰动,机头偏向左或右时,此时作用在垂直安定面上的气动力就会产生一个与偏转方向相反的力矩,使飞机恢复到原来的 ...
Stabilizer (aeronautics) - Wikipedia
网页In the conventional aircraft configuration, separate vertical (fin) and horizontal stabilizers form an empennage positioned at the tail of the aircraft. Other arrangements of the empennage, such as the V-tail configuration, feature stabilizers which contribute to a combination of longitudinal and directional stabilization and control.
Design Process: V-Tails - KITPLANES
网页2022年9月14日 · A V-tail is a configuration where the horizontal stabilizer and vertical fin are replaced by a pair of surfaces mounted at a high dihedral angle (usually about 45°). Because these angled surfaces can produce both vertical force and side force, the two V-tail surfaces can replace the three surfaces of a conventional tail.
A comprehensive review of vertical tail design - ResearchGate
网页2016年9月12日 · This work deals with a comprehensive review of vertical tail design methods for aircraft directional stability and vertical tail sizing.
Design Process: Vertical Tail Functions–Yaw Stability and Damping
网页2022年5月13日 · A vertical tail design that generates significant yaw damping at post-stall angles of attack will help give the airplane benign spin characteristics. The directional stabilization and yaw damping of the vertical tail play a major role in determining the open-loop lateral/directional characteristics.
网页vertical tail design (i.e. spin recovery) that the effect of horizontal tail into vertical tail is investigated. The details on each step will be introduced in the later sections. The purpose of this chapter is to provide design considerations, …
Creating the Vertical Tail – OpenVSP Ground School - NASA
网页2022年10月27日 · In this tutorial we will demonstrate how to add a vertical tail to your model and ensure that the tail intersects the fuselage while matching the three-view planform. Topics include rotating wing components and wing symmetry.
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