The thesis has the purpose of implementing a tool for a preliminary design of a helicopter. The tool is asoftware developed in Matlab and executes the calculations based on two theories: momentum and blade element. With this tool the flight performancescan be calculated, from hover to maximum forward speed, of three types of helicopter:conventional, coaxial and tandem. For sizing of each rotor configuration, the power required, forward velocities, range and endurance can be calculated
Preliminary design tool of conventional/coaxial/tandem helicopters
Cojocari, Anatol
2017/2018
Abstract
The thesis has the purpose of implementing a tool for a preliminary design of a helicopter. The tool is asoftware developed in Matlab and executes the calculations based on two theories: momentum and blade element. With this tool the flight performancescan be calculated, from hover to maximum forward speed, of three types of helicopter:conventional, coaxial and tandem. For sizing of each rotor configuration, the power required, forward velocities, range and endurance can be calculatedFile in questo prodotto:
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/28533