Atnaujinkite slapukų nuostatas

El. knyga: Flight Stability and Control

DRM apribojimai

  • Kopijuoti:

    neleidžiama

  • Spausdinti:

    neleidžiama

  • El. knygos naudojimas:

    Skaitmeninių teisių valdymas (DRM)
    Leidykla pateikė šią knygą šifruota forma, o tai reiškia, kad norint ją atrakinti ir perskaityti reikia įdiegti nemokamą programinę įrangą. Norint skaityti šią el. knygą, turite susikurti Adobe ID . Daugiau informacijos  čia. El. knygą galima atsisiųsti į 6 įrenginius (vienas vartotojas su tuo pačiu Adobe ID).

    Reikalinga programinė įranga
    Norint skaityti šią el. knygą mobiliajame įrenginyje (telefone ar planšetiniame kompiuteryje), turite įdiegti šią nemokamą programėlę: PocketBook Reader (iOS / Android)

    Norint skaityti šią el. knygą asmeniniame arba „Mac“ kompiuteryje, Jums reikalinga  Adobe Digital Editions “ (tai nemokama programa, specialiai sukurta el. knygoms. Tai nėra tas pats, kas „Adobe Reader“, kurią tikriausiai jau turite savo kompiuteryje.)

    Negalite skaityti šios el. knygos naudodami „Amazon Kindle“.

Aircraft safety is a function of several parameters including flight stability and control. An air vehicle must be stable if it is to remain in flight. Moreover, it must be controllable as well as trimmable. This book delivers the fundamental concepts of stability and control, as well as their associated areas. It explains airworthiness, dynamic and static stability, longitudinal, lateral, and directional control, flight measurement devices and sensors, and control surfaces which are necessary topics to be considered during the aircraft design process. This book is mainly focused on air vehicles' stability features and control capabilities. The aircraft addressed in this book is a rigid-body point mass object. Describing the complete motion of a rigid-body aircraft, this book covers equations of motion with six degrees of freedom (DOF)
 Preface.- Aircraft Equations.- Trim.- Longitudinal Stability.-
Lateral-directional Stability.- Longitudinal Control.- latera;-Directional
Control.-Problems.- References.
Mohammad Sadraey has over twenty years of teaching experience at a number of institutions including Southern New Hampshire University, Daniel Webster College, and the University of Kansas. He has both an M.Sc. and Ph.D. in Aerospace Engineering in 2006. He is a senior member of the American  Institute of Aeronautics and Astronautics (AIAA), member of Sigma Gamma Tu, and the American Society for Engineering Education (ASEE).