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

Journal Journal of Aeronautics & Aerospace Engineering
ISSN: 2168-9792
Output data Year: 2017, Volume: 6:1, Number: 1000183, Pages: 1-15 Pages count : 15
Tags Calculation aerodynamic characteristics of the aircraft, AN-225; Thrust required and thrust available; Practical ceiling of aircraft; Building a polar flight; Flight dynamics.
Authors Ahmed Soliman M E 1
Affiliations
1 NSTU

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.
Cite: 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.
Dates:
Submitted: Feb 10, 2017
Accepted: Mar 6, 2017
Published print: Mar 10, 2017
Identifiers: No identifiers
Citing: Пока нет цитирований