alexa Calculation of the Flight Characteristics of the Aircraft, AN-225
ISSN: 2168-9792

Journal of Aeronautics & Aerospace Engineering
Open Access

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Research Article

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

Ahmed Soliman M.Sherif*

Novosibirsk State Technical University, Russia

*Corresponding Author:
Ahmed Soliman M.Sherif
Researcher, Novosibirsk State Technical University
pr. Karla Marksa, 20, Novosibirsk, Novosibirskaya-oblast', Russia
Tel: +7(952)900-64-61
E-mail: [email protected]

Received Date: February 10, 2017; Accepted Date: March 06, 2017; Published Date: March 10, 2017

Citation: Ahmed Soliman M.Sherif (2017) Calculation of the Flight Characteristics of the Aircraft, AN-225. J Aeronaut Aerospace Eng 6:183. doi: 10.4172/2168- 9792.1000183

Copyright: © 2017 Ahmed Soliman M.Sherif. This is an open-access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.

 

Abstract

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.

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