Principles of Helicopter Aerodynamics with CD ExtraCambridge University Press, 24 апр. 2006 г. - Всего страниц: 826 Written by an internationally recognized teacher and researcher, this book provides a thorough, modern treatment of the aerodynamic principles of helicopters and other rotating-wing vertical lift aircraft such as tilt rotors and autogiros. The text begins with a unique technical history of helicopter flight, and then covers basic methods of rotor aerodynamic analysis, and related issues associated with the performance of the helicopter and its aerodynamic design. It goes on to cover more advanced topics in helicopter aerodynamics, including airfoil flows, unsteady aerodynamics, dynamic stall, and rotor wakes, and rotor-airframe aerodynamic interactions, with final chapters on autogiros and advanced methods of helicopter aerodynamic analysis. Extensively illustrated throughout, each chapter includes a set of homework problems. Advanced undergraduate and graduate students, practising engineers, and researchers will welcome this thoroughly revised and updated text on rotating-wing aerodynamics. |
Содержание
A History of Helicopter Flight | 1 |
Fundamentals of Rotor Aerodynamics | 55 |
Blade Element Analysis | 115 |
Rotating Blade Motion | 171 |
Helicopter Performance | 212 |
Aerodynamic Design of Helicopters | 277 |
Aerodynamics of Rotor Airfoils | 347 |
Unsteady Airfoil Behavior | 423 |
Dynamic Stall | 525 |
Rotor Wakes and Blade Tip Vortices | 567 |
RotorAirframe Interactional Aerodynamics | 655 |
Autogiros and Gyroplanes | 692 |
Aerodynamics of Wind Turbines | 723 |
Computational Methods for Helicopter Aerodynamics | 771 |
Appendix 815 | 816 |
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Часто встречающиеся слова и выражения
advance ratio aircraft airfoil sections airframe airspeed American Helicopter Soc angle of attack approximation autogiro autorotation BEMT blade element blade flapping blade pitch blade tip blade twist boundary layer C₁ camber chord Cierva coaxial rotor collective pitch computational convected density altitude disk loading drag dynamic stall effects engine equation experimental figure of merit flow separation force forward flight function fuselage gust helicopter rotor hinge hover increase indicial induced power induced velocity inflow interactions leading edge Leishman lift coefficient linear Mach number main rotor measurements methods momentum theory NACA nondimensional operating pitching moment power required predictions pressure problem produced relatively Reynolds number rotational rotor blades rotor disk rotor performance rotor power rotor thrust rotor wake shown in Fig solution surface tail rotor tip speed tip vortex tip vortices turbulent unsteady aerodynamic values vortex ring wake model wind turbine
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