IHS ESDU Non-dimensional methods for the measurement of level-flight performance of turbine-engined helicopters. 74042

Description
ESDU 74042 shows how the method of ESDU 73026 is applied to analyse flight test measured data on level-flight performance. 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 73027 shows the method of ESDU 73026 applied to analyse hover flight-measured performance.
Description
ESDU 74042 shows how the method of ESDU 73026 is applied to analyse flight test measured data on level-flight performance. 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 73027 shows the method of ESDU 73026 applied to analyse hover flight-measured performance.

Suppliers

Company
Product
Description
Supplier Links
Non-dimensional methods for the measurement of level-flight performance of turbine-engined helicopters. - 74042 - IHS ESDU
London, United Kingdom
Non-dimensional methods for the measurement of level-flight performance of turbine-engined helicopters.
74042
Non-dimensional methods for the measurement of level-flight performance of turbine-engined helicopters. 74042
ESDU 74042 shows how the method of ESDU 73026 is applied to analyse flight test measured data on level-flight performance. 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 73027 shows the method of ESDU 73026 applied to analyse hover flight-measured performance.

ESDU 74042 shows how the method of ESDU 73026 is applied to analyse flight test measured data on level-flight performance. 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 73027 shows the method of ESDU 73026 applied to analyse hover flight-measured performance.

Buy Now

Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 74042
Product Name Non-dimensional methods for the measurement of level-flight performance of turbine-engined helicopters.
Unlock Full Specs
to access all available technical data

Similar Products