Aircraft_performance

Aircraft performance

Aircraft performance

Aspect of aeronautical design and mission planning


Aircraft performance refers to the ability of airplanes and helicopters to accomplish certain useful things.[1] It is an important consideration when designing and testing aircraft, to ensure the aircraft can be operated in an efficient and economic manner.[2] There are typically trade-offs involved, for example an aircraft optimised for cruise performance will not necessarily be optimised for the climb.[3] Adaptive compliant wings and variable-sweep wings are technologies aimed at improving performance during the different stages of flight.

The subject of aircraft performance includes aircraft speed, ceiling, range and fuel efficiency, take-off distance required, and climb rate. It also includes aircraft controllability speeds.[4]

Aircraft manufacturers will publish performance data in an aircraft flight manual, concerning the behaviour of the aircraft under various circumstances, such as different speeds, weights, and air temperatures, pressures, & densities.[5][6] Performance data is information pertaining to takeoff, climb, range, endurance, descent, and landing.[1]

Aircraft performance is affected by atmospheric conditions. Climb performance will be reduced in hot and high conditions, as well as in humid conditions. Higher temperatures and humidities, and lower pressures reduce air density.[1]

See also


References

  1. Federal Aviation Administration: "Pilot's Handbook of Aeronautical Knowledge", Chapter 11.
  2. Saarlas, Maido (2007). Aircraft performance. Hoboken, N.J.: John Wiley. ISBN 978-0-470-04416-2.
  3. Joshi, Shiv; Tidwell, Zeb; Crossley, William; Ramakrishnan, Sekaripuram (2004-04-19). "Comparison of Morphing Wing Strategies Based upon Aircraft Performance Impacts". 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. doi:10.2514/6.2004-1722. ISBN 978-1-62410-079-6.
  4. McCormick, Barnes W. (1 August 1979). "7. Airplane Performance". Aerodynamics, Aeronautics and Flight Mechanics. Wiley. ISBN 978-0-471-03032-4. Retrieved 6 July 2022.



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