Advanced configurations for very large transport airplanes by J. H. McMasters, I. M. Kroo
By J. H. McMasters, I. M. Kroo
Plane layout 1 (1998) 217}242
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;Fairey IIIF [Aircraft Profile 044] КНИГИ ;ВОЕННАЯ ИСТОРИЯ Название: Fairey IIIF Автор: Francis okay. Mason Серия: plane Profile 044 Издательство: Profile guides Ltd Страниц:12 Формат: PDF в rarЯзык: английский Размер: four. 39 Мб Для сайта: Мир книгСамолеты Fairey IIIF строились в четырех основных вариантах, но среди них были многочисленные вариации с различным оборудованием и разными типами конструкций (смешанными или цельнометаллическими).
The Fairey Rotodyne was once a wide British compound helicopter designed and outfitted by means of the Fairey Aviation corporation and meant for advertisement and army purposes. It was once thought of to be one of many iconic aviation tasks of the 1950s/60s and a shiny destiny used to be deliberate for the plane. generally authorised to be a progressive layout, it used to be economically practicable, quickly and able to vertical take-off and touchdown from urban centre heliports.
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Additional resources for Advanced configurations for very large transport airplanes
When a helicopter is hovering, the tail rotor is operating in very disturbed airflow. As the helicopter achieves ETL, the tail rotor begins to generate much more thrust because of the less disturbed airflow. The helicopter reacts to the increased thrust by yawing. Therefore, as the helicopter achieves ETL, you must reduce tail rotor thrust by pedal input at about the same time that you need to make cyclic adjustments for lateral tracking, acceleration, and climb. Induced Flow As the rotor blades rotate, they generate what is called rotational relative wind.
A helicopter in forward flight, or hovering with a headwind or crosswind, has more molecules of air entering the aft portion of the rotor blade. Therefore, the angle of attack is less and the induced flow is greater at the rear of the rotor disk. 2-22 Resultant Resultant Lift Lift Thrust Thrust Drag Drag Helicopter movement Resultant Figure 2-41. Forces acting on the helicopter during sideward flight. when maneuvering the helicopter sideways to avoid such hazards from happening. Refer to Chapter 11, Helicopter Hazards and Emergencies.
If the amount of lift is greater than the actual weight, the helicopter accelerates upwards until the lift force equals the weight gain altitude; if thrust is less than weight, the helicopter accelerates downward. When operating near the ground, the effects of the proximity to the surface change this response. The drag of a hovering helicopter is mainly induced drag incurred while the blades are producing lift. There is, however, some profile drag on the blades as they rotate through the air and a small amount of parasite drag from the non-lift-producing surfaces of the helicopter, such as the rotor hub, cowlings, and 2-13 landing gear.