Calculation of the Flight Characteristics of the Aircraft, AN-225 | Sciact

Calculation of the Flight Characteristics of the Aircraft, AN-225 Научная публикация

Журнал

Journal of Aeronautics & Aerospace Engineering
ISSN: 2168-9792

Вых. Данные

Год: 2017, Том: 6:1, Номер: 1000183, Страницы: 1-15 Страниц : 15

Ключевые слова

Calculation aerodynamic characteristics of the aircraft, AN-225; Thrust required and thrust available; Practical ceiling of aircraft; Building a polar flight; Flight dynamics.

Авторы

Ahmed Soliman M E ¹

Организации

NSTU

Flight dynamics - The science of the laws of motion of aircraft under the influence of wind, gravity, and reaction forces. It is a combination of mainly three classic disciplines: solid mechanics, fluid dynamics, and mathematics. Among the wide range of problems in the dynamics of flight of great practical importance are the problems connected with the study of the steady rectilinear motion of the aircraft. The solution allows them to determine the flight characteristics of the aircraft, characterized by the range of possible speeds and heights, rate of climb, range, flight time, and so on.

Ahmed Soliman M.E.
Calculation of the Flight Characteristics of the Aircraft, AN-225
Journal of Aeronautics & Aerospace Engineering. 2017. V.6:1. N1000183. P.1-15.

Поступила в редакцию:	10 февр. 2017 г.
Принята к публикации:	6 мар. 2017 г.
Опубликована в печати:	10 мар. 2017 г.

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