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What is the angle that measures 170 degrees?
It is an obtuse angle. It is an obtuse angle. It is an obtuse angle. It is an obtuse angle.
What is the negation of angle a is a right angle?
It is: "angle a is not a right angle" or "angle a is greater than or less than a right angle".
Supplements of the same angle are congruent what's the best statement for reason 6 of this proof?
angle B and angle D are supplements, angle B is congruent to angle D, angle A is congruent to angle A, or angle A is congruent to angle C
what type of angle is angle 98?
An angle of 98 degrees is an obtuse angle
What type of angle is a 12 degree angle?
A 12 degree angle is an acute angle.
Why high angle of attack is used in fighter air crafts?
Dear sir,The followings are my quest....1. what is angle of attack?2. what is high angle of attack?3. why high angle of attack is used in super sonic air crafts?4. control measures used in high angle of attack?answer me through mail.yours ,isaacaeroisaac@gmail.com
What is an angle of attack?
An angle of attack is the angle between the chord line of an airfoil and the airflow over it.
What is the angle of attack on an airplane?
The angle of attack is an aerodynamic term which refers to the angle between the mean wing chord of the airfoil and the direction of airflow. This is different from the pitch angle of the aircraft in that the pitch angle refers to the aircrafts position in relation to the horizon, whereas angle of attack refers to the aircrafts angle in relation to airflow.
How does angle of attack affect lift and drag?
A higher angle of attack has an increase of both lift and drag.
What is the difference between the angle of attack and angle of incidence?
Zero degrees.
What is the angle between the airplanes wing and the direction of airflow called?
The angle between the airplane's wing and the direction of airflow is called the angle of attack. This angle is important for generating lift and controlling the aircraft's flight.
What is the point at which lift starts to drop off?
This is termed the Critical Angle of Attack and represents a maximum in the Lift Coefficient vs. Angle of Attack curve. If the angle of attack is increased beyond this point, the wing will stall. For most airfoils, the critical angle of attack is around 15 deg. For swept back wings it is typically higher.
What control stall margin?
Stall margin is the difference in the critical angle of attack and the angle of attack in which you are operating.Example:Suppose, critical angle of attack= 15°AOA operating in a flight= 5°then, Lift by the wing balances the weight of the airplane with a STALL MARGIN= 10°Stall Margin is being controlled by an angle of attack and the position of flap control..CHEERS!
How does the angle of attack affect the accuracy of attack in fencing?
the steeper the angle of attack the easier it is for your opponent to pare' your thrust or lunge. the steeper the angle of attack, the less your thrust is lined up with your line of sight, giving a larger emphasis on depth perception in the attack, and in a stressed, rushed situation, that often results in the touch being either high or low.
What will happen to the boundary layer when the angle of attack increases?
When the angle of attack increases, the boundary layer will thicken and separate from the surface of the airfoil earlier, leading to increased drag and reduced lift. This can eventually lead to flow separation and stall if the angle of attack is too high.
The upward angle of the wing is called the?
angle of attack. It is the angle between the chord line of the wing and the oncoming airflow. A higher angle of attack generates more lift but also increases drag.
What is the difference between the Angle of Attack and th Angle of Incidence?
Hi!The angle of incidence is built into the aircraft, and cannot be changed. This angle is the angle that the wing makes with a level surface (such as if the ground if the aircraft were parked).The angle of attack (commonly abbreviated AoA), is the angle that the chordline of the airfoil makes with the relative wind. So if you were in straight and level flight, maintaining altitude, the angle of attack would be zero degrees.When an aircraft exceeds a critical angle of attack (which is determined by the design of the airplane), the airflow will peel off of the wing, causing the wing to stop producing lift. The aircraft is, in this scenario, stalled.Hope this helps.Source(s):PPL ASEL 6/17/08
