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Dynamics of aircraft flight

Record Type:	Electronic resources : Monograph/item
Title/Author:	Dynamics of aircraft flightGilles Louis.
Author:	Louis, Gilles.
Published:	London :ISTE ;2022.
Description:	1 online resource :ill.
Subject:	Flight.
Online resource:	https://onlinelibrary.wiley.com/doi/book/10.1002/9781119988281
ISBN:	9781119988281$q(electronic bk.)

Dynamics of aircraft flight
Louis, Gilles.

Dynamics of aircraft flight[electronic resource] /Gilles Louis. - London :ISTE ;2022. - 1 online resource :ill. - Systems and industrial engineering series. - Systems and industrial engineering series..

Includes bibliographical references and index.

Performance calculations can be classified into three main types: lift, thrust and slope. Firstly, since the lift profile is known and unmodifiable from the time an aircraft is designed, the mass at a given speed or the speed at a given mass must be determined. Then, once the thrust of the engines and the mass are known, the slope must be calculated. Finally, once the slope is known (for example, level flight) as well as the mass, it is necessary to deduce the thrust; this is the position of the throttle control lever that ensures balance. The corresponding consumption must then be defined. Performance specifications for customer aircraft, such as manoeuvrability, fuel consumption, maintenance, safety and testability, have become ever more demanding with each generation of equipment. Major technical advances have been required: wing profiles, engines, materials to reduce mass, etc. This book presents a theoretical approach to flight mechanics that makes it possible to grasp the subject and links it with the empirical approach of manufacturers.

ISBN: 9781119988281$q(electronic bk.)

Standard No.: 10.1002/9781119988281doiSubjects--Topical Terms:

265324
Flight.

LC Class. No.: TL570

Dewey Class. No.: 629.132/3

Dynamics of aircraft flight
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003 OCoLC
005 20220810124436.0
006 m o d
007 cr cnu---unuuu
008 240227s2022 enka ob 001 0 eng d
020 $a 9781119988281$q(electronic bk.)
020 $a 1119988284$q(electronic bk.)
020 $z 9781786307194$q(print)
024 7 $a 10.1002/9781119988281 $2 doi
035 $a 1336937497
040 $a DG1 $b eng $c DG1
041 0 $a eng
050 4 $a TL570
082 0 4 $a 629.132/3 $2 23
100 1 $a Louis, Gilles. $3 960525
245 1 0 $a Dynamics of aircraft flight $h [electronic resource] / $c Gilles Louis.
260 $a London : $b ISTE ; $a Hoboken, NJ : $b Wiley, $c 2022.
300 $a 1 online resource : $b ill.
490 1 $a Systems and industrial engineering series
504 $a Includes bibliographical references and index.
520 $a Performance calculations can be classified into three main types: lift, thrust and slope. Firstly, since the lift profile is known and unmodifiable from the time an aircraft is designed, the mass at a given speed or the speed at a given mass must be determined. Then, once the thrust of the engines and the mass are known, the slope must be calculated. Finally, once the slope is known (for example, level flight) as well as the mass, it is necessary to deduce the thrust; this is the position of the throttle control lever that ensures balance. The corresponding consumption must then be defined. Performance specifications for customer aircraft, such as manoeuvrability, fuel consumption, maintenance, safety and testability, have become ever more demanding with each generation of equipment. Major technical advances have been required: wing profiles, engines, materials to reduce mass, etc. This book presents a theoretical approach to flight mechanics that makes it possible to grasp the subject and links it with the empirical approach of manufacturers.
588 $a Description based on print version record.
650 0 $a Flight. $3 265324
650 0 $a Aeronautics. $3 276530
830 0 $a Systems and industrial engineering series. $3 754807
856 4 0 $u https://onlinelibrary.wiley.com/doi/book/10.1002/9781119988281