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Pondlife
Pondlife
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Induced Is an increase in induced drag is just product becausealways caused by an increase in the angle of increased AoAattack?

In INDUCED DRAG VIDEOthis video at 2:57

Look at video at 2:57 they increase the AoA to compensatemaintain lift,and which normally than larger AoA will increase drag ,(becuasealso increases the drag increase with increasing AoA).Imagine Now, imagine that we dontdon't increase the AoA,drag: the drag will not increase but we will not have enough lift to keepto maintain level flight.. But if If we want to keep the same lift and fly in level flight we must increase the AoA,so only then drag will increase..

So :

1)to increase induced drag, must be and ASSUMPTION -"FOR SAME LIFT", otherwise dragonly then will not increase because we didntthe drag increase AoA....

2)InducedSo induced drag is just caused by a larger AoA,so basicly so basically this is a type of pressure drag..

Do you agree that if we dontdon't increase the AoA(at 2:57 on as described in the video) than then the drag will not increase as well? So do you agree if we comapare drag between 2D and 3D wing we must have ASSUMPTION-"FOR SAME LIFT"?

Induced drag is just product because of increased AoA?

INDUCED DRAG VIDEO

Look at video at 2:57 they increase AoA to compensate lift,and normally than larger AoA will increase drag ,(becuase drag increase with increasing AoA).Imagine that we dont increase AoA,drag will not increase but we will not have enough lift to keep level flight.. But if we want keep same lift and fly in level flight we must increase AoA,so only then drag will increase..

So :

1)to increase induced drag, must be ASSUMPTION -"FOR SAME LIFT", otherwise drag will not increase because we didnt increase AoA....

2)Induced drag is just caused by larger AoA,so basicly this is type of pressure drag..

Do you agree that if we dont increase AoA(at 2:57 on video) than drag will not increase as well? So do you agree if we comapare drag between 2D and 3D wing we must have ASSUMPTION-"FOR SAME LIFT"?

Is an increase in induced drag always caused by an increase in the angle of attack?

In this video at 2:57 they increase the AoA to maintain lift, which normally also increases the drag. Now, imagine that we don't increase the AoA: the drag will not increase but we will not have enough lift to maintain level flight. If we want to keep the same lift and fly in level flight we must increase the AoA and only then will the drag increase.

So induced drag is just caused by a larger AoA, so basically this is a type of pressure drag.

Do you agree that if we don't increase the AoA as described in the video then the drag will not increase as well?

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ROTOR
ROTOR
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INDUCED DRAG VIDEO

Look at video at 2:57 they increase AoA to compensate lift,and normally than larger AoA will increase drag ,(becuase drag increase with increasing AoA).Imagine that we dont increase AoA,drag will not increase but we will not have enough lift to keep level flight.. But if we want keep same lift and fly in level flight we must increase AoA,so only then drag will increase..

So :

1)to increase induced drag, must be ASSUMPTION -"FOR SAME LIFT", otherwise drag will not increase because we didnt increase AoA....

2)Induced drag is just caused by larger AoA,so basicly this is type of pressure drag..

Do you agree that if we dont increase AoA(at 2:57 on video) than drag will not increase as well and do? So do you agree that induced dragif we comapare drag between 2D and 3D wing we must have ASSUMPTION-"FOR SAME LIFT"?

INDUCED DRAG VIDEO

Look at video at 2:57 they increase AoA to compensate lift,and normally than larger AoA will increase drag ,(becuase drag increase with increasing AoA).Imagine that we dont increase AoA,drag will not increase but we will not have enough lift to keep level flight.. But if we want keep same lift and fly in level flight we must increase AoA,so only then drag will increase..

So :

1)to increase induced drag, must be ASSUMPTION -"FOR SAME LIFT", otherwise drag will not increase because we didnt increase AoA....

2)Induced drag is just caused by larger AoA,so basicly this is type of pressure drag..

Do you agree that if we dont increase AoA(at 2:57 on video) than drag will not increase as well and do you agree that induced drag must have ASSUMPTION-"FOR SAME LIFT"?

INDUCED DRAG VIDEO

Look at video at 2:57 they increase AoA to compensate lift,and normally than larger AoA will increase drag ,(becuase drag increase with increasing AoA).Imagine that we dont increase AoA,drag will not increase but we will not have enough lift to keep level flight.. But if we want keep same lift and fly in level flight we must increase AoA,so only then drag will increase..

So :

1)to increase induced drag, must be ASSUMPTION -"FOR SAME LIFT", otherwise drag will not increase because we didnt increase AoA....

2)Induced drag is just caused by larger AoA,so basicly this is type of pressure drag..

Do you agree that if we dont increase AoA(at 2:57 on video) than drag will not increase as well? So do you agree if we comapare drag between 2D and 3D wing we must have ASSUMPTION-"FOR SAME LIFT"?

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ROTOR
ROTOR
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  • 1
  • 9

Induced drag is just product because of increased AoA?

INDUCED DRAG VIDEO

Look at video at 2:57 they increase AoA to compensate lift,and normally than larger AoA will increase drag ,(becuase drag increase with increasing AoA).Imagine that we dont increase AoA,drag will not increase but we will not have enough lift to keep level flight.. But if we want keep same lift and fly in level flight we must increase AoA,so only then drag will increase..

So :

1)to increase induced drag, must be ASSUMPTION -"FOR SAME LIFT", otherwise drag will not increase because we didnt increase AoA....

2)Induced drag is just caused by larger AoA,so basicly this is type of pressure drag..

Do you agree that if we dont increase AoA(at 2:57 on video) than drag will not increase as well and do you agree that induced drag must have ASSUMPTION-"FOR SAME LIFT"?