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  2. Energy–maneuverability theory - Wikipedia

    en.wikipedia.org/wiki/Energy–maneuverability...

    Energy–maneuverability theory is a model of aircraft performance. It was developed by Col. John Boyd , a fighter pilot, and Thomas P. Christie , a mathematician with the United States Air Force , [ 1 ] and is useful in describing an aircraft's performance as the total of kinetic and potential energies or aircraft specific energy .

  3. Ground effect (aerodynamics) - Wikipedia

    en.wikipedia.org/wiki/Ground_effect_(aerodynamics)

    Flight Theory and Aerodynamics. Hoboken, New Jersey: John Wiley & Sons, Inc. ISBN 978-0-471-37006-2. Gleim, Irving (1982). Pilot Flight Maneuvers. Ottawa, Ontario, Canada: Aviation Publications. ISBN 0-917539-00-1. Pilot's Encyclopedia of Aeronautical Knowledge (Federal Aviation Administration). New York: Skyhorse Publishing, 2007. ISBN 1-60239 ...

  4. Aircraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_dynamics

    In many flight dynamics applications, the Earth frame is assumed to be inertial with a flat x E,y E-plane, though the Earth frame can also be considered a spherical coordinate system with origin at the center of the Earth. The other two reference frames are body-fixed, with origins moving along with the aircraft, typically at the center of gravity.

  5. History of aerodynamics - Wikipedia

    en.wikipedia.org/wiki/History_of_aerodynamics

    Although the modern theory of aerodynamic science did not emerge until the 18th century, its foundations began to emerge in ancient times. The fundamental aerodynamics continuity assumption has its origins in Aristotle's Treatise on the Heavens, although Archimedes, working in the 3rd century BC, was the first person to formally assert that a fluid could be treated as a continuum. [1]

  6. High-speed flight - Wikipedia

    en.wikipedia.org/wiki/High-speed_flight

    In subsonic aerodynamics, the theory of lift is based upon the forces generated on a body and a moving gas (air) in which it is immersed. At airspeeds below about 260 kn (480 km/h; 130 m/s; 300 mph), air can be considered incompressible in regards to an aircraft, in that, at a fixed altitude , its density remains nearly constant while its ...

  7. Flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Flight_dynamics

    The flight dynamics of spacecraft differ from those of aircraft in that the aerodynamic forces are of very small, or vanishingly small effect for most of the vehicle's flight, and cannot be used for attitude control during that time. Also, most of a spacecraft's flight time is usually unpowered, leaving gravity as the dominant force.

  8. Aerodynamics - Wikipedia

    en.wikipedia.org/wiki/Aerodynamics

    Forces of flight on a powered aircraft in unaccelerated level flight. Understanding the motion of air around an object (often called a flow field) enables the calculation of forces and moments acting on the object. In many aerodynamics problems, the forces of interest are the fundamental forces of flight: lift, drag, thrust, and weight. Of ...

  9. Aeronautics - Wikipedia

    en.wikipedia.org/wiki/Aeronautics

    The science of aerodynamics deals with the motion of air and the way that it interacts with objects in motion, such as an aircraft. The study of aerodynamics falls broadly into three areas: Incompressible flow occurs where the air simply moves to avoid objects, typically at subsonic speeds below that of sound (Mach 1).