# Which placement of Wing gives more longitudinal stability of aircraft?

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The position of the centre of gravity (CG). As a rule of thumb, the further forward (towards the nose) the CG, the more stable the aircraft with respect to pitching.

## What gives an aircraft longitudinal stability?

The longitudinal static stability of an aircraft is significantly influenced by the distance (moment arm or lever arm) between the centre of gravity (c.g.) and the aerodynamic centre of the airplane. The c.g. is established by the design of the airplane and influenced by its loading, as by payload, passengers, etc.

## What provides stability along the longitudinal axis?

Longitudinal Stability:

Straight wings (negative) Wing Sweep (positive) Fuselage (negative) Horizontal stabilizer (largest positive)

## What is the most stable wing design?

The elliptical wing is aerodynamically most efficient because elliptical spanwise lift distribution induces the lowest possible drag.

## Which structure provides longitudinal stability to a fixed wing aircraft?

This is known as directional stability. The vertical stabilizer usually serves as the base to which the rudder is attached. The horizontal stabilizer provides stability of the aircraft about its lateral axis. This is known as longitudinal stability.

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## How do you improve longitudinal stability?

To obtain static longitudinal stability, the relation of the wing and tail moments must be such that, if the moments are initially balanced and the airplane is suddenly nosed up, the wing moments and tail moments will change so that the sum of their forces will provide an unbalanced but restoring moments which in turn, …

## Why is forward cg more stable?

A forward CG with the increase in stability will make it easier to recover from a stall, however moving the CG forward will also increase drag and with drag comes a reduction in cruise speeds and fuel efficiency.

## What provides the lateral stability of aircraft?

Lateral static stability is concerned with the ability of the aircraft to maintain wings-level equilibrium in the roll sense. Wing dihedral is the most visible parameter which confers lateral static stability on an aircraft, although there are many other contributions, some of which are destabilising.

## How does a high wing aircraft achieve roll stability?

For the high wing aircraft, the center of gravity sits below the wing, meaning the fuselage of the aircraft acts as a pendulum to increase roll stability relative to the low wing aircraft, whose center of gravity is balanced above the wing.

## Which placement of wing gives minimum drag to the aircraft?

The minimum drag configuration puts the elevator in front. For stable flight, the elevator should be configured so that it changes lift faster than the main wing, damping out disturbances in angle of attack.

## Where should wings be on a plane?

To control and maneuver the aircraft, smaller wings are located at the tail of the plane. The tail usually has a fixed horizontal piece, called the horizontal stabilizer, and a fixed vertical piece, called the vertical stabilizer.

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## Which of the wing configurations has the highest stability?

High wing aircraft are more stable because of their lower center of gravity CG) , relative to the wing. The gravity hangs underneath the lift of the wings.

## Why is longitudinal stability about the lateral axis?

Stability about the airplane’s longitudinal axis, which extends form nose to tail, is called lateral stability. This helps to stabilize the lateral or rolling effect when one wing gets lower than the wing on the opposite side of the airplane.

## What aircraft design feature gives an aircraft longitudinal stability?

Thrust line affects longitudinal stability. Power or thrust can also have a destabilizing effect in that an increase of power may tend to make the nose rise. The aircraft designer can offset this by establishing a “high thrust line” wherein the line of thrust passes above the CG.

## What is lateral and longitudinal stability?

[153] Longitudinal stability and control is concerned with an airplane’s pitching motion, lateral stability and control relates to an airplane’s rolling motion, and directional stability and control relates to an airplane’s yawing motion.