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FREE ESSAY ON FLIGHT

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Flights AA 808
A description of the crash of American Airways Flight 808 in 1993. -- 1,605 words; MLA

Flight Crew Management
An examination of a new form of management known as crew resource management as applied to flight crew management in a time of stress. -- 4,158 words; MLA

Hess's Flight to England in 1941
An examination of the controversy surrounding the flight of Nazi Germany's Deputy Fuhrer Rudolf Hess to Scotland on May 10, 1941. -- 3,481 words; MLA

Evolution Of Bird Flight
Examines fossil evidence, leg modification into wings, conflicting theories, dynamics of flight, non-flying birds and reasons for flight. -- 1,800 words;

Japan Airlines - The Crash of Flight 123
This paper serves as a report detailing the air disaster involving Japan Airlines Flight number 123. -- 1,356 words; MLA

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FLIGHT

Research: Airplanes are an efficient way of traveling to far places. Airplanes are amazing
if you know what and how the air keeps the plane airborne. There are three components of
flight: aerodynamics, the Bernoulli principal and supersonic flight. Some other things
about flight are the four forces, lift, drag, weight, and thrust. One of the basic things
you need to know about airplanes is that the places where the plane can balance on one
point called the center of gravity. The tail on the plane is needed to balance the
pitching movement. First of all, aerodynamics plays a major role on many things,
especially in airplanes. Aerodynamics is the reaction of the air on the specially shaped
wing that lifts an airplane off the ground. Also, aerodynamics is the study of gases in
motion. The term aerodynamics comes from the Greeks meaning air power. Isaac Newton bases
aerodynamics on the physics theorem. People who experiment with aerodynamics are called
aerodynamicist. Their basic tool is the wind tunnel. A professor of engineering, Osborne
Reynolds, conducted many experiments with paper airplanes and regular airplanes and found
out Viscosity (thickness) affects the way fluids behave. All fluids have some viscosity.
As a fluid flows over a surface, the fluid molecules closest to the surface cling
microscopic roughness of the surface. As you move away from the surface, there is a small
transition distance where the fluid's viscosity limits the change in speed of the
adjacent molecules, until at a certain distances the fluid is at full speed. (Paper
airplane aerodynamics www.geocities.com/capecanaveral/1817/paene/html) Osborne invented a
number that was devised which gives the importance of viscosity in fluid flow. It's
called the Reynold's number. Reynold's number =9340 for air so you'd take 9340x velocity
relative to surface (mph) x length over surface fluid has traveled feet. This determines
how influential the viscosity is. Secondly, Swiss mathematician and physicist, Daniel
Bernoulli, created Bernoulli's principle in 1738. It stated the concept that as the speed
of a moving fluid increases, the pressure within the fluid decreases. An increase in the
fluid's speed must be matched by a decrease in pressure. The mathematical theorem for the
Bernoulli affect is p + ? p V2. One source said, "the principle also applies to the
spinning of a baseball" (Simons, 1989, pg. 23) The rotation causes an additional velocity
component to be sent in the direction of rotation. Because of all that, the total
velocity around the ball is higher on one side then the other. This is an example of how
Bernoulli's principle works. Next, supersonic flight includes speeds from mach one to
five: above five are considered hypersonic. The bell X-1 rocket plane first achieved
supersonic flight in 1947. "Many attempts had been made before that but when the plane
ran against the sound barrier the pilot often lost control when the shock waves built up
against the surface" (Compton's 1994). Mach one is considered traveling below the speed
of sound (subsonic). Mach two is traveling twice the speed of sound (supersonic). All
aircraft's that are traveling at supersonic or hypersonic speed create a shock wave that
represents a big change in the air pressure. The shock is in reality a cone shape (a mach
cone). The mach cone at mach 1 is more of a hill but as the mach numbers increase, the
cone gets pushed back to more of a mountain. As the wave gets closer to the wing, the
drag increases dramatically. When you are at subsonic mach numbers, the drag is increased
as a result of small wing span or low aspect ratio. "Low aspect ratio is the ratio of
span to mean chord of an airfoil" (Reithmaier, 1995). A typical supersonic airplane gives
off two main shock waves: bow shock and tail shock. Next, there are four forces of
flight; lift, weight, drag, and thrust. Drag is the air resistance to forward motion.
Thrust is produced by the power plant that contracts drag. The formula for drag is D=1/2
x p x V2 x S x CD. The S in this formula is the area of the wing area of the whole
aircraft. If the plane is level, lift will equal weight. In conclusion, airplanes have a
lot of scientific information behind the way that the plane stays in the air. The
airplanes have to be aerodynamically shaped to reach supersonic flight. The Bernoulli
affect also helps keep the plane in the air by measuring the viscosity and comparing it
to the air pressure. Supersonic flight is from mach 1 to mach 5 and above that is
hypersonic. This relates to my experiment in many ways. The paper airplane has to be
aerodynamically shaped so it can fly well. The paper airplane also has a Reynolds number,
which was created by Daniel Bernoulli. The equation for paper airplane is 9340*10*.4
=37,000. Of course the project airplane will not be traveling at supersonic speeds but it
would have the same concept of cutting through the air.


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