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Yes, the launching Angle of Attack, along with the launching force, will determine range, unless there is some outside force (such as a motor) to accommodate it.
Throw it at an angle to the horizontal.
An angle of attack is the angle between the chord line of an airfoil and the airflow over it.
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.
a paper airplane will run out of momentum, momentum (speed, vertical speed is required for the airflow over the wings to generate lift, a too high angle of attack (nose high) will cause disrupt airflow over the wings and the plane will stall
The amounts depend on the airplane's size, shape, speed, altitude, and angle of attack, among other things.
The plane stall remain the same regardless of gross weight.
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!
An airplane's fuselage affects it flight by a lot. It can change its speed, maneuverability, angle of attack, and even its necessary-for-flight wing size.
Do not exceed the critical angle of attack, basically the angle the wings make with the oncoming air as the plane moves forward.
As trust increases, speed increases. Providing the angle of attack, and the wind speed stay the same.
The effect of a hole on a paper airplane would depend on the type of paper airplane the hole is on, and where it is on the aircraft.