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An understanding of flight is rooted in a strong grasp of how an airplane gets in the air—and stays there. Both a passenger jet and a tiny paper airplane are governed by the same forces. Understanding airplane aerodynamics is key to a successful partnership with the atmosphere: They are the foundation for study for student pilots , an instinctive part of work life for engineers and everyday aviators, and a pathway to comprehension and relaxation for white-knuckle travelers. You may be surprised to hear that aerodynamics applies to objects that never leave a runway at all. Where those in the aviation industry are concerned, however, aerodynamics applies to how the forces of flight act on an aircraft. We need help! When the Wright Brothers were designing their first Flyer , they took careful note of how the birds along the North Carolina coast wheeled and glided on the ocean wind. They understood that, unlike people, birds were built to manage four important forces: weight, lift, thrust, and drag. These four staples of aerodynamics are constantly working in opposition to one another. Airplanes and Aerodynamics

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Airplanes and Aerodynamics Video

Private Pilot Tutorial 4: Aerodynamics of Flight (Part 1 of 3)

As noted on page the rocket motor is the only current example of aeronautical interest in Class II of propulsive systems.

Since it does not work by accelerating atmospheric air, it cannot be treated by Froude's momentum theory. It is unique among current aircraft power plants in that it can operate independently of air from the atmosphere. The consequences of this are:.

In a rocket, some form of chemical is converted in the combustion chamber into gas at high temperature and pressure, which is then exhausted at supersonic speed through a nozzle. Suppose a rocket to be travelling at a speed of V, and let the gas leave the nozzle with a speed of v relative to the rocket.

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Whilst in the tanks the mean m of fuel has a forward momentum of mV. After discharge from the nozzle the gas has a rearward momentum of m v — V. Thus the thrust depends only on the rate of fuel Airplanes and Aerodynamics and the Aerodyanmics of discharge relative to the rocket. The thrust does not depend on the speed of the rocket itself. In particular, the possibility exists that the speed of the rocket Fcan exceed the speed of the gas relative to both the rocket, v, and relative to the axes of reference, v — V.

Thus the rate of change of kinetic energy is d E. Thus the propulsive efficiency of the rocket is.

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