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An analysis of the efficiency of coanda - notar anti-torque systems for small helicoptersThe use of jet thrust for anti-torque for monorotor small helicopters is based on thecirculation control concept, which result in a distributed side force along the entire tail boomassembly....
général - core.ac.uk - PDF: core.ac.uk
Eme'ioying a tail boom and three horizontal-tail positions... The con-figurations had sweptback wings and tail surfaces and a tail boom of rectangular cross section....
Aerodynamic effect of strakes on two-dimensional tail boom models of the oh-58a and the oh-58d helicoptersDuring hover and low speed flight, helicopters experience significant aerodynamic forces on the tail boom caused by the wake from the main and tail rotors and by crosswinds....
Production of a helicopter tail boom and associated mechanical tests... One of the uses of these materials is for the tail boom of helicopters....
Simulation of tail boom vibrations using main rotor-fuselage computational fluid dynamics (cfd)...this work, fully-resolved rotor-fuselage interactional aerodynamics is used as the forcing term in a model based on the Euler-Bernoulli equation, aiming to simulate helicopter tail-boom vibration....

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