IHS ESDU Drag and pressure recovery characteristics of auxiliary air inlets at subsonic speeds. 86002

Description
ESDU 86002 provides methods for estimating the drag and pressure recovery of intakes partially or wholly immersed in the boundary layer. The methods, which are semi-empirical, apply to circular, semi-circular or rectangular scoop intakes, with or without boundary layer diverter, and flush rectangular intakes having a shallow entrance ramp of rectangular or NACA curved-divergent planform. The effect of throat just aft of the lip is derived from theoretical calculations taking account of the velocity profile. Empirical methods, based on a limited database, predicted spillage drag and, for scoop intakes, the contribution from profile drag.
Description
ESDU 86002 provides methods for estimating the drag and pressure recovery of intakes partially or wholly immersed in the boundary layer. The methods, which are semi-empirical, apply to circular, semi-circular or rectangular scoop intakes, with or without boundary layer diverter, and flush rectangular intakes having a shallow entrance ramp of rectangular or NACA curved-divergent planform. The effect of throat just aft of the lip is derived from theoretical calculations taking account of the velocity profile. Empirical methods, based on a limited database, predicted spillage drag and, for scoop intakes, the contribution from profile drag.

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Drag and pressure recovery characteristics of auxiliary air inlets at subsonic speeds. - 86002 - IHS ESDU
London, United Kingdom
Drag and pressure recovery characteristics of auxiliary air inlets at subsonic speeds.
86002
Drag and pressure recovery characteristics of auxiliary air inlets at subsonic speeds. 86002
ESDU 86002 provides methods for estimating the drag and pressure recovery of intakes partially or wholly immersed in the boundary layer. The methods, which are semi-empirical, apply to circular, semi-circular or rectangular scoop intakes, with or without boundary layer diverter, and flush rectangular intakes having a shallow entrance ramp of rectangular or NACA curved-divergent planform. The effect of throat just aft of the lip is derived from theoretical calculations taking account of the velocity profile. Empirical methods, based on a limited database, predicted spillage drag and, for scoop intakes, the contribution from profile drag.

ESDU 86002 provides methods for estimating the drag and pressure recovery of intakes partially or wholly immersed in the boundary layer. The methods, which are semi-empirical, apply to circular, semi-circular or rectangular scoop intakes, with or without boundary layer diverter, and flush rectangular intakes having a shallow entrance ramp of rectangular or NACA curved-divergent planform. The effect of throat just aft of the lip is derived from theoretical calculations taking account of the velocity profile. Empirical methods, based on a limited database, predicted spillage drag and, for scoop intakes, the contribution from profile drag.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 86002
Product Name Drag and pressure recovery characteristics of auxiliary air inlets at subsonic speeds.
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