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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.
Historical Review
Determination of Tandem Wing Aircraft Aerodynamic Characteristics
Effect of Geometric Parameters on Aerodynamic Characteristics
Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft
Conclusions