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Dynamics of aircraft flight

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Dynamics of aircraft flight/ Gilles Louis.
作者:	Louis, Gilles.
出版者:	London :ISTE ; : 2022.,
面頁冊數:	1 online resource :ill.
標題:	Flight. -
電子資源:	https://onlinelibrary.wiley.com/doi/book/10.1002/9781119988281
ISBN:	9781119988281

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

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

532570
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
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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 3674630
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 532570
650 0 $a Aeronautics. $3 560293
830 0 $a Systems and industrial engineering series. $3 2204728
856 4 0 $u https://onlinelibrary.wiley.com/doi/book/10.1002/9781119988281