Book description
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.
Table of contents
- Cover
- Title Page
- List of Contributors
- Series Preface
- Preface
- Companion Website
- 1 Advanced UAV Aerodynamics, Flight Stability and Control
-
2 Aerodynamics of UAV Configurations
- 2.1 Introduction
- 2.2 Emerging Technologies in UAV Aerodynamics
- 2.3 Aerodynamics and Stealth Compromises
- 2.4 Rotor Blade Tip Aerodynamics
- 2.5 Flight Dynamics of Canard Aircraft
- 2.6 Aerodynamics of the UCAV 1303 Delta‐wing Configuration
- 2.7 Flow Structure Modification using Plasma Actuators
- 2.8 Conclusion
- References
-
Part I: Novel Concepts in Unmanned Aircraft Aerodynamics
-
1.1 Fixed‐wing (airplanes)
-
3 Aerodynamic Performance Analysis of Three Different Unmanned Re‐entry Vehicles
- 3.1 Introduction
- 3.2 Vehicle Description
- 3.3 Flight Scenario and Flow‐regime Assessment
- 3.4 Rarefied and Transitional Regimes
- 3.5 Viscous‐interaction Regime
- 3.6 High‐temperature Real‐gas Regime
- 3.7 Laminar‐to‐turbulent Transition Assessment
- 3.8 Design Approach and Tools
- 3.9 Aerodynamic Characterization
- 3.10 Low‐order Methods Aerodynamic Results
- 3.11 CFD‐based Aerodynamic Results
- References
- 4 Nonlinear Reduced‐order Aeroservoelastic Analysis of Very Flexible Aircraft
- 5 Unmanned Aircraft Wind Tunnel Testing
- 6 Chord‐dominated Ground‐effect Aerodynamics of Fixed‐wing UAVs
-
3 Aerodynamic Performance Analysis of Three Different Unmanned Re‐entry Vehicles
-
1.2 Rotary‐wing (helicopter)
- 7 Dynamics Modelling and System Identification of Small Unmanned Helicopters
- 8 Aerodynamic Derivative Calculation Using Radial Basis Function Neural Networks
- 9 Helicopter BERP Tip
- 10 Framework for the Optimisation of a Helicopter Rotor Blade with an Approximate BERP Tip
- 11 Active Blade Twist in Rotary UAVs using Smart Actuation
- 1.3 Hybrid Aircraft
-
1.1 Fixed‐wing (airplanes)
-
Part II: Novel Concepts in Unmanned Aircraft Flight Stability and Control
-
2.1 Fixed‐wing (airplanes)
- 13 Closed‐loop Active Flow Control for UAVs
- 14 Autonomous Gust Alleviation in UAVs
- 15 Virtual Flight Simulation using Computational Fluid Dynamics
- 16 Flow Structure Modification Using Plasma Actuation for Enhanced UAV Flight Control
- 17 Constrained Motion Planning and Trajectory Optimization for Unmanned Aerial Vehicles
- 18 Autonomous Space Navigation Using Nonlinear Filters with MEMS Technology
- 19 Adaptive Fault‐tolerant Attitude Control for Spacecraft Under Loss of Actuator Effectiveness
-
2.1 Fixed‐wing (airplanes)
- 2.2 Quad‐rotor Aircraft
- Index
- End User License Agreement
Product information
- Title: Advanced UAV Aerodynamics, Flight Stability and Control
- Author(s):
- Release date: April 2017
- Publisher(s): Wiley
- ISBN: 9781118928684
You might also like
book
Basic Helicopter Aerodynamics, 3rd Edition
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to the first principles …
book
Helicopter Flight Dynamics, 3rd Edition
The Book The behaviour of helicopters and tiltrotor aircraft is so complex that understanding the physical …
book
Military Avionics Systems
Ian Moir and Allan Seabridge Military avionics is a complex and technically challenging field which requires …
book
Aircraft Propulsion, 2nd Edition
New edition of the successful textbook updated to include new material on UAVs, design guidelines in …