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.
In a paper airplane experiment, the independent variable is the factor that is being deliberately manipulated or changed by the researcher. This could be the type of paper used, the design of the paper airplane, the angle of launch, or the force applied when throwing the airplane.
An angle of attack is the angle between the chord line of an airfoil and the airflow over it.
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.
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.
The aerodynamic design of a paper airplane affects its ability to generate lift and reduce drag, which are essential for flight. Factors such as wing shape, size, and angle of attack impact how air flows around the airplane, allowing it to stay airborne and travel further. By optimizing these design elements, a paper airplane can achieve better flight performance.
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.
Paper airplanes fly due to the principles of aerodynamics. When a paper airplane is thrown, the shape of its wings and the angle at which it is thrown create lift, which allows the airplane to stay in the air and glide. The force of gravity pulling the airplane down is counteracted by the lift generated by the wings, allowing the airplane to fly.
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!