What is the offset in a seaplane's hull?
$begingroup$
I noticed there is a little offset in a seaplane's hull (highlighted in the following picture). I suppose this is useful as it exists in all the seaplanes I know. It seems it does not help hydrodynamics neither aerodynamics. I could not find any clue by myself as I don't know this feature's name.
My question, what is its name and purpose?
(wikimedia.org)
aircraft-design feature-identification fuselage seaplane
edited 5 hours ago
ymb1
69.6k7221369
asked 5 hours ago
Manu HManu H
5,5101058136
$endgroup$
add a comment |
$begingroup$
I noticed there is a little offset in a seaplane's hull (highlighted in the following picture). I suppose this is useful as it exists in all the seaplanes I know. It seems it does not help hydrodynamics neither aerodynamics. I could not find any clue by myself as I don't know this feature's name.
My question, what is its name and purpose?
(wikimedia.org)
aircraft-design feature-identification fuselage seaplane
edited 5 hours ago
ymb1
69.6k7221369
asked 5 hours ago
Manu HManu H
5,5101058136
$endgroup$
add a comment |
$begingroup$
I noticed there is a little offset in a seaplane's hull (highlighted in the following picture). I suppose this is useful as it exists in all the seaplanes I know. It seems it does not help hydrodynamics neither aerodynamics. I could not find any clue by myself as I don't know this feature's name.
My question, what is its name and purpose?
(wikimedia.org)
aircraft-design feature-identification fuselage seaplane
edited 5 hours ago
ymb1
69.6k7221369
asked 5 hours ago
Manu HManu H
5,5101058136
$endgroup$
I noticed there is a little offset in a seaplane's hull (highlighted in the following picture). I suppose this is useful as it exists in all the seaplanes I know. It seems it does not help hydrodynamics neither aerodynamics. I could not find any clue by myself as I don't know this feature's name.
My question, what is its name and purpose?
(wikimedia.org)
aircraft-design feature-identification fuselage seaplane
aircraft-design feature-identification fuselage seaplane
edited 5 hours ago
ymb1
69.6k7221369
asked 5 hours ago
Manu HManu H
5,5101058136
edited 5 hours ago
ymb1
69.6k7221369
asked 5 hours ago
Manu HManu H
5,5101058136
edited 5 hours ago
ymb1
69.6k7221369
edited 5 hours ago
ymb1
69.6k7221369
edited 5 hours ago
ymb1
69.6k7221369
69.6k7221369
asked 5 hours ago
Manu HManu H
5,5101058136
asked 5 hours ago
Manu HManu H
5,5101058136
asked 5 hours ago
Manu HManu H
5,5101058136
5,5101058136
add a comment |
add a comment |
2 Answers
2
active
oldest
votes
$begingroup$
That's called the step. Without it, you'd have to fight against the buoyancy of the rear end of the hull when you rotate for takeoff.
However, a seaplane float or hull must be designed to permit the seaplane to be rotated or pitched up to increase the wing's angle of attack and gain the most lift for takeoffs and landings. Thus, the underside of the float or hull has a sudden break in its longitudinal lines at the approximate point around which the seaplane rotates into the lift off attitude. This break, called a "step," also provides a means of interrupting the capillary or adhesive properties of the water.
The water can then flow freely behind the step, resulting in minimum surface friction so the seaplane can lift out of the water. The steps are located slightly behind the airplane's centre of gravity, approximately at the point where the main wheels of a landplane are located. If the steps were located to far aft or forward of this point, it would be difficult, if not impossible, to rotate the airplane into a pitch-up attitude prior to planing (rising partly out of the water while moving at high speed) or lift off. Although steps are necessary, the sharp break along the float's or hull's underside causes structural stress concentration, and in flight produces considerable drag because of the eddying turbulence it creates in the airflow.
answered 5 hours ago
HobbesHobbes
3,9021016
$endgroup$
add a comment |
$begingroup$
It's called a hull step. Below is with and without:
It reduces water drag. As the plane gains speed and the aft body is lifted, only the forward hull will be in contact with the water.
Source: Laté 631 Replica - Chapter 3 - Hydrodynamics
answered 5 hours ago
ymb1ymb1
69.6k7221369
$endgroup$
add a comment |
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2 Answers
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2 Answers
2
active
oldest
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active
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active
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votes
$begingroup$
That's called the step. Without it, you'd have to fight against the buoyancy of the rear end of the hull when you rotate for takeoff.
However, a seaplane float or hull must be designed to permit the seaplane to be rotated or pitched up to increase the wing's angle of attack and gain the most lift for takeoffs and landings. Thus, the underside of the float or hull has a sudden break in its longitudinal lines at the approximate point around which the seaplane rotates into the lift off attitude. This break, called a "step," also provides a means of interrupting the capillary or adhesive properties of the water.
The water can then flow freely behind the step, resulting in minimum surface friction so the seaplane can lift out of the water. The steps are located slightly behind the airplane's centre of gravity, approximately at the point where the main wheels of a landplane are located. If the steps were located to far aft or forward of this point, it would be difficult, if not impossible, to rotate the airplane into a pitch-up attitude prior to planing (rising partly out of the water while moving at high speed) or lift off. Although steps are necessary, the sharp break along the float's or hull's underside causes structural stress concentration, and in flight produces considerable drag because of the eddying turbulence it creates in the airflow.
answered 5 hours ago
HobbesHobbes
3,9021016
$endgroup$
add a comment |
$begingroup$
That's called the step. Without it, you'd have to fight against the buoyancy of the rear end of the hull when you rotate for takeoff.
However, a seaplane float or hull must be designed to permit the seaplane to be rotated or pitched up to increase the wing's angle of attack and gain the most lift for takeoffs and landings. Thus, the underside of the float or hull has a sudden break in its longitudinal lines at the approximate point around which the seaplane rotates into the lift off attitude. This break, called a "step," also provides a means of interrupting the capillary or adhesive properties of the water.
The water can then flow freely behind the step, resulting in minimum surface friction so the seaplane can lift out of the water. The steps are located slightly behind the airplane's centre of gravity, approximately at the point where the main wheels of a landplane are located. If the steps were located to far aft or forward of this point, it would be difficult, if not impossible, to rotate the airplane into a pitch-up attitude prior to planing (rising partly out of the water while moving at high speed) or lift off. Although steps are necessary, the sharp break along the float's or hull's underside causes structural stress concentration, and in flight produces considerable drag because of the eddying turbulence it creates in the airflow.
answered 5 hours ago
HobbesHobbes
3,9021016
$endgroup$
add a comment |
$begingroup$
That's called the step. Without it, you'd have to fight against the buoyancy of the rear end of the hull when you rotate for takeoff.
However, a seaplane float or hull must be designed to permit the seaplane to be rotated or pitched up to increase the wing's angle of attack and gain the most lift for takeoffs and landings. Thus, the underside of the float or hull has a sudden break in its longitudinal lines at the approximate point around which the seaplane rotates into the lift off attitude. This break, called a "step," also provides a means of interrupting the capillary or adhesive properties of the water.
The water can then flow freely behind the step, resulting in minimum surface friction so the seaplane can lift out of the water. The steps are located slightly behind the airplane's centre of gravity, approximately at the point where the main wheels of a landplane are located. If the steps were located to far aft or forward of this point, it would be difficult, if not impossible, to rotate the airplane into a pitch-up attitude prior to planing (rising partly out of the water while moving at high speed) or lift off. Although steps are necessary, the sharp break along the float's or hull's underside causes structural stress concentration, and in flight produces considerable drag because of the eddying turbulence it creates in the airflow.
answered 5 hours ago
HobbesHobbes
3,9021016
$endgroup$
That's called the step. Without it, you'd have to fight against the buoyancy of the rear end of the hull when you rotate for takeoff.
However, a seaplane float or hull must be designed to permit the seaplane to be rotated or pitched up to increase the wing's angle of attack and gain the most lift for takeoffs and landings. Thus, the underside of the float or hull has a sudden break in its longitudinal lines at the approximate point around which the seaplane rotates into the lift off attitude. This break, called a "step," also provides a means of interrupting the capillary or adhesive properties of the water.
The water can then flow freely behind the step, resulting in minimum surface friction so the seaplane can lift out of the water. The steps are located slightly behind the airplane's centre of gravity, approximately at the point where the main wheels of a landplane are located. If the steps were located to far aft or forward of this point, it would be difficult, if not impossible, to rotate the airplane into a pitch-up attitude prior to planing (rising partly out of the water while moving at high speed) or lift off. Although steps are necessary, the sharp break along the float's or hull's underside causes structural stress concentration, and in flight produces considerable drag because of the eddying turbulence it creates in the airflow.
answered 5 hours ago
HobbesHobbes
3,9021016
answered 5 hours ago
HobbesHobbes
3,9021016
answered 5 hours ago
HobbesHobbes
3,9021016
answered 5 hours ago
HobbesHobbes
3,9021016
3,9021016
add a comment |
add a comment |
$begingroup$
It's called a hull step. Below is with and without:
It reduces water drag. As the plane gains speed and the aft body is lifted, only the forward hull will be in contact with the water.
Source: Laté 631 Replica - Chapter 3 - Hydrodynamics
answered 5 hours ago
ymb1ymb1
69.6k7221369
$endgroup$
add a comment |
$begingroup$
It's called a hull step. Below is with and without:
It reduces water drag. As the plane gains speed and the aft body is lifted, only the forward hull will be in contact with the water.
Source: Laté 631 Replica - Chapter 3 - Hydrodynamics
answered 5 hours ago
ymb1ymb1
69.6k7221369
$endgroup$
add a comment |
$begingroup$
It's called a hull step. Below is with and without:
It reduces water drag. As the plane gains speed and the aft body is lifted, only the forward hull will be in contact with the water.
Source: Laté 631 Replica - Chapter 3 - Hydrodynamics
answered 5 hours ago
ymb1ymb1
69.6k7221369
$endgroup$
It's called a hull step. Below is with and without:
It reduces water drag. As the plane gains speed and the aft body is lifted, only the forward hull will be in contact with the water.
Source: Laté 631 Replica - Chapter 3 - Hydrodynamics
answered 5 hours ago
ymb1ymb1
69.6k7221369
answered 5 hours ago
ymb1ymb1
69.6k7221369
answered 5 hours ago
ymb1ymb1
69.6k7221369
answered 5 hours ago
ymb1ymb1
69.6k7221369
69.6k7221369
add a comment |
add a comment |
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