IHS ESDU Approximate parametric method for propeller thrust estimation. Addendum A: application to fixed-pitch propellers. 83028

Description
ESDU 83028, which is an Addendum to ESDU 83001, provides an approximate method for determining the uninstalled static thrust and the thrust lapse characteristics for a wide range of direct-drive, fixed-pitch propellers operating at airspeeds up to 250 kn. The method applies at airspeeds above and below that at which the propeller-engine combination reaches maximum rotational speed. The ranges of values of propeller design parameters are disc loadings from 2 to 8 hp/sq ft (16 to 64 kW/sq m), tip speeds from 700 to 1000 ft/s (200 to 300 m/s), and total activity factors from 160 to 540.
Description
ESDU 83028, which is an Addendum to ESDU 83001, provides an approximate method for determining the uninstalled static thrust and the thrust lapse characteristics for a wide range of direct-drive, fixed-pitch propellers operating at airspeeds up to 250 kn. The method applies at airspeeds above and below that at which the propeller-engine combination reaches maximum rotational speed. The ranges of values of propeller design parameters are disc loadings from 2 to 8 hp/sq ft (16 to 64 kW/sq m), tip speeds from 700 to 1000 ft/s (200 to 300 m/s), and total activity factors from 160 to 540.

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Approximate parametric method for propeller thrust estimation.  Addendum A: application to fixed-pitch propellers. - 83028 - IHS ESDU
London, United Kingdom
Approximate parametric method for propeller thrust estimation. Addendum A: application to fixed-pitch propellers.
83028
Approximate parametric method for propeller thrust estimation. Addendum A: application to fixed-pitch propellers. 83028
ESDU 83028, which is an Addendum to ESDU 83001, provides an approximate method for determining the uninstalled static thrust and the thrust lapse characteristics for a wide range of direct-drive, fixed-pitch propellers operating at airspeeds up to 250 kn. The method applies at airspeeds above and below that at which the propeller-engine combination reaches maximum rotational speed. The ranges of values of propeller design parameters are disc loadings from 2 to 8 hp/sq ft (16 to 64 kW/sq m), tip speeds from 700 to 1000 ft/s (200 to 300 m/s), and total activity factors from 160 to 540.

ESDU 83028, which is an Addendum to ESDU 83001, provides an approximate method for determining the uninstalled static thrust and the thrust lapse characteristics for a wide range of direct-drive, fixed-pitch propellers operating at airspeeds up to 250 kn. The method applies at airspeeds above and below that at which the propeller-engine combination reaches maximum rotational speed. The ranges of values of propeller design parameters are disc loadings from 2 to 8 hp/sq ft (16 to 64 kW/sq m), tip speeds from 700 to 1000 ft/s (200 to 300 m/s), and total activity factors from 160 to 540.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 83028
Product Name Approximate parametric method for propeller thrust estimation. Addendum A: application to fixed-pitch propellers.
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