A 6 page paper. This essay discusses a number of aspects related to helicopter flight. The issues and conditions discussed include how the craft achieves lift, the effect of the air flowing over the blades, torque, drag and centrifugal force. The effects of transverse flow and settling with power are also included in the discussion. The writer incorporates Bernoulli's effect and Newton's laws throughout the essay. Bibliography lists 10 sources.
Name of Research Paper File: MM12_PGchptf.RTF
Unformatted Sample Text from the Research Paper:
include how the craft achieves lift, the effect of the air flowing over the blades, torque, drag and centrifugal force. The effects of transverse flow and settling with power are
also included in the discussion. The writer incorporates Bernoullis effect and Newtons laws throughout the essay. There has been an ongoing debate about whether the Bernoulli effect
or principle should even be considered when discussing airplanes and helicopters or whether only Newtons laws of motions should be considered. It would seem that both are important to understand
how helicopters fly. Some argue that the main lift for the aircraft is gained because the wing has an upward angle which forces the air hitting the underside of the
wing forces it downward (Eastlake, 2007). It is Newtons third law that has to do with reaction force that provides the lift (Eastlake, 2007). Bernoullis principle is generally explained
using a venturi tube, which is a cylindrical tube that is squashed in the middle (ALLSTAR, 2004). The principle states that as a fluid passes through this tube, when it
reaches the smaller opening, the squashed part, the fluid gains speed as it passes through (ALLSTAR, 2004). In other words, as the fluid passes through the smaller part of the
tube, it increases velocity while it decreases pressure. Air is a fluid so the principle applies to air. The reason for the extra speed has to do with the
energy needed for the molecules to pass through the squished part of the tube, which, in turn reduces the pressure (ALLSTAR, 2004). The pressure changes so that it is different
at one point than at the other point (ALLSTAR, 2004). As the pressure decreases over the top of the rotor blade, lift is achieved (ALLSTAR, 2004). Airfoils, (wings and rotor