LEADER 02438nam 2200481 450 001 9910829890103321 005 20221205224110.0 010 $a1-119-98827-6 010 $a1-119-98828-4 010 $a1-119-98826-8 035 $a(MiAaPQ)EBC6992832 035 $a(Au-PeEL)EBL6992832 035 $a(CKB)22444730000041 035 $a(OCoLC)1319650258 035 $a(OCoLC-P)1319650258 035 $a(CaSebORM)9781786307194 035 $a(EXLCZ)9922444730000041 100 $a20221205d2022 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aDynamics of aircraft flight /$fGilles Louis 210 1$aLondon :$cISTE Ltd,$d[2022] 210 4$dİ2022 215 $a1 online resource (204 pages) 311 08$aPrint version: Louis, Gilles Dynamics of Aircraft Flight Newark : John Wiley & Sons, Incorporated,c2022 9781786307194 320 $aIncludes bibliographical references and index. 330 $aPerformance 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. 606 $aFlight 606 $aAeronautics 615 0$aFlight. 615 0$aAeronautics. 676 $a629.1323 700 $aLouis$b Gilles$01665907 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910829890103321 996 $aDynamics of aircraft flight$94024854 997 $aUNINA