This book contains extensive data about tandem wing aircraft. It includes a review of modern flying vehicles with four fixed wings, a review of analytical, numerical and experimental methods; results of the studies about aerodynamics; dependencies between geometrical parameters and aerodynamic characteristics, practical recommendations in development and optimizing of tandem wing aircraft to provide high lift-to-drag ratio, stability, and controllability. This is an ideal book for graduate students, researchers, and engineers working in fields of aerodynamics and conceptual design of the aircraft especially UAVs, ground-effect vehicles, and convertiplanes.
Inhaltsverzeichnis
Chapter 1. Historical Review. - Chapter 2. Determination of Tandem Wing Aircraft Aerodynamic Characteristics. - Chapter 3. Effect of Geometric Parameters on Aerodynamic Characteristics. - Chapter 4. Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft.
