DYNAMICS OF AIRCRAFT FLIGHT

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 a...

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Bibliographic Details
Main Author: LOUIS, GILLES.
Format: Electronic
Language: English
Published: [S.l.] : JOHN WILEY, 2022.
Subjects:
Flight.
Aeronautics.
elektronické knihy
electronic books
ISBN: 9781119988267
1119988268
1786307197
9781786307194
Physical Description: 1 online resource

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LEADER 02348cam a2200325 4500
001 kn-on1319650258
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 220524s2022 xx o 0|| 0 eng d
040 |a YDX  |b eng  |c YDX  |d SFB  |d ORMDA  |d OCLCF  |d OCLCQ  |d N$T  |d OCLCO  |d OCLCQ  |d EBLCP 
020 |a 9781119988267  |q (electronic bk.) 
020 |a 1119988268  |q (electronic bk.) 
020 |z 1786307197 
020 |z 9781786307194 
035 |a (OCoLC)1319650258  |z (OCoLC)1319827991  |z (OCoLC)1321799974 
100 1 |a LOUIS, GILLES. 
245 1 0 |a DYNAMICS OF AIRCRAFT FLIGHT  |h [electronic resource]. 
260 |a [S.l.] :  |b JOHN WILEY,  |c 2022. 
300 |a 1 online resource 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
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. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Flight. 
650 0 |a Aeronautics. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
776 0 8 |i Print version:  |z 1786307197  |z 9781786307194  |w (OCoLC)1314429715 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpDAF00022/dynamics-of-aircraft?kpromoter=marc  |y Full text 

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