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Worldtech
A NACA 0012 airfoil having a chord of \(2.3\,m\) is in an airstream velocity of \(70\,m/s\) at standard sea level conditions. Find the angle of attack for this airfoil, if the lift per unit span produced is \(1400\,N\).
airfoil
airspeed
lift
lift coefficient
lift force
on 22nd July 2021 in
Aeronautics.
1K
1
0
Kisan Kumar
Can an airfoil fly upside-down ?
airfoil
lift
lift and drag
lift coefficient
lift force
on 13th July 2021 in
Aerodynamics.
2K
1
0
techAir
Find the gliding distance of an aircraft flying at an altitude of \(1500\,m\) with a maximum lift to drag ratio of \(8\).
Airplane design
drag force
lift and drag
lift force
on 3rd February 2021 in
Aeronautics.
1K
1
0
Worldtech
Airfoil Terminology and NACA Series of airfoil Nomenclature.
Aircraft performance
airfoil
Airplane design
airspeed
lift force
on 10th December 2020 in
Flight mechanics.
1K
1
0
Kisan Kumar
What is canard in an aircraft?
Aircraft performance
Airplane design
canard
lift force
on 1st July 2020 in
Flight mechanics.
1K
1
0
Worldtech
Lift and Drag forces on aircraft
drag
drag force
lift
lift and drag
lift force
on 15th May 2020 in
Aerospace.
1K
1
0
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