Question
A helicopter with a rotor diameter of 10.3 m is hovering at sea-level in an ISA. The rotor rotates at 650 rpm and the induced
A helicopter with a rotor diameter of 10.3 m is hovering at sea-level in an ISA. The
rotor rotates at 650 rpm and the induced air velocity through the rotor is 26 m/s.
Calculate the thrust coefficient.
We don't have thrust, so how do we calculate thrust coefficient?
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Shigleys Mechanical Engineering Design
Authors: Richard G. Budynas, J. Keith Nisbett
9th edition
77679520, 73529281, 1259986241, 978-0077679521, 9780073529288, 9781259986246, 978-1121345317
