Aircraft: Design, Technology and Safety


Collin Parker (Editor)

Series: Transportation Issues, Policies and R&D
BISAC: TEC002000

In early stages of an aircraft design process, it is necessary to determine the minimum thrust or power requirement and rapidly select the appropriate propulsion, which involves a tight coupling between flight performance and missions’ analyses, engine performance prediction and design optimization.

The first chapter of this book provides an overview of how to determine the minimum thrust or power requirements for jet and propeller driver transport aircraft. The second chapter examines the comprehensive modeling and design of production processes of aircraft assembly. The final chapter focuses on the computational modeling of the Be-200 and Be-103 amphibious aircraft models.
(Imprint: Nova)

Table of Contents

Table of Contents


Chapter 1
Power Requirements for Transport Aircrafts
(Adel Ghenaiet, Faculty of Mechanical and Process Engineering, University of Sciences and Technology, USTHB, BP32 El-Alia, Bab-Ezzouar, Algiers, Algeria)

Chapter 2
Comprehensive Modeling and Design of Production Processes of Aircraft Assembly
(Rozhdestvensky Aleksandr V., Samsonov Oleg S., “MATI” – Russian State University of Aviation Technology, Russia)

Chapter 3
Computational Modeling of Amphibious Aircraft Be-200 and Be-103
(Iftikhar B. Abbasov, V’iacheslav V. Orekhov, and Gennady S. Panatov, Engineering-Technological Academy of the Southern Federal University,
per. Nekrasovskyi, Taganrog, Russia)



Publish with Nova Science Publishers

We publish over 800 titles annually by leading researchers from around the world. Submit a Book Proposal Now!