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Основной контент книги Advanced UAV Aerodynamics, Flight Stability and Control
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Raamatu kestus 787 lehekülge

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Advanced UAV Aerodynamics, Flight Stability and Control

Novel Concepts, Theory and Applications
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Raamatut ei saa failina alla laadida, kuid seda saab lugeda meie rakenduses või veebis.

€170,34

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Comprehensively covers emerging aerospace technologies 

Advanced UAV aerodynamics, flight stability and control: Novel concepts, theory and applications presents emerging aerospace technologies in the rapidly growing field of unmanned aircraft engineering. Leading scientists, researchers and inventors describe the findings and innovations accomplished in current research programs and industry applications throughout the world. Topics included cover a wide range of new aerodynamics concepts and their applications for real world fixed-wing (airplanes), rotary wing (helicopter) and quad-rotor aircraft.

The book begins with two introductory chapters that address fundamental principles of aerodynamics and flight stability and form a knowledge base for the student of Aerospace Engineering. The book then covers aerodynamics of fixed wing, rotary wing and hybrid unmanned aircraft, before introducing aspects of aircraft flight stability and control.

Key features:

Sound technical level and inclusion of high-quality experimental and numerical data. Direct application of the aerodynamic technologies and flight stability and control principles described in the book in the development of real-world novel unmanned aircraft concepts. Written by world-class academics, engineers, researchers and inventors from prestigious institutions and industry. The book provides up-to-date information in the field of Aerospace Engineering for university students and lecturers, aerodynamics researchers, aerospace engineers, aircraft designers and manufacturers.

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Vanusepiirang:
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Ilmumiskuupäev Litres'is:
05 juuli 2018
Objętość:
787 lk
ISBN:
9781118928714
Üldsuurus:
68 МБ
Lehekülgede koguarv:
787
Kustija:
Õiguste omanik:
John Wiley & Sons Limited
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