IHS ESDU Non-dimensional methods for the measurement of hover performance of turbine-engined helicopters. 73027

Description
ESDU 73027 shows how the method of ESDU 73026 is applied to analyse flight test measured data on hover. Three possible techniques are available. If rotor speed cannot be varied, Mach number effects are ignored and only density is required to characterise the atmosphere; otherwise temperature and either pressure or density must be measured. Collective pitch can be measured instead of using the torquemeter to measure power. A complete worked example based on practical test data illustrates the method. ESDU 74042 shows the method of ESDU 73026 applied to analyse level flight measured performance.
Description
ESDU 73027 shows how the method of ESDU 73026 is applied to analyse flight test measured data on hover. Three possible techniques are available. If rotor speed cannot be varied, Mach number effects are ignored and only density is required to characterise the atmosphere; otherwise temperature and either pressure or density must be measured. Collective pitch can be measured instead of using the torquemeter to measure power. A complete worked example based on practical test data illustrates the method. ESDU 74042 shows the method of ESDU 73026 applied to analyse level flight measured performance.

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Non-dimensional methods for the measurement of hover performance of turbine-engined helicopters. - 73027 - IHS ESDU
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Non-dimensional methods for the measurement of hover performance of turbine-engined helicopters.
73027
Non-dimensional methods for the measurement of hover performance of turbine-engined helicopters. 73027
ESDU 73027 shows how the method of ESDU 73026 is applied to analyse flight test measured data on hover. Three possible techniques are available. If rotor speed cannot be varied, Mach number effects are ignored and only density is required to characterise the atmosphere; otherwise temperature and either pressure or density must be measured. Collective pitch can be measured instead of using the torquemeter to measure power. A complete worked example based on practical test data illustrates the method. ESDU 74042 shows the method of ESDU 73026 applied to analyse level flight measured performance.

ESDU 73027 shows how the method of ESDU 73026 is applied to analyse flight test measured data on hover. Three possible techniques are available. If rotor speed cannot be varied, Mach number effects are ignored and only density is required to characterise the atmosphere; otherwise temperature and either pressure or density must be measured. Collective pitch can be measured instead of using the torquemeter to measure power. A complete worked example based on practical test data illustrates the method. ESDU 74042 shows the method of ESDU 73026 applied to analyse level flight measured performance.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 73027
Product Name Non-dimensional methods for the measurement of hover performance of turbine-engined helicopters.
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