IHS ESDU Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds. 75028

Description
ESDU 75028 gives curves, derived from a correlation of experimental data, that enable the drag increment to be predicted due to a groove of planform aspect ratio greater than 8 normal to the flow. For grooves inclined at angles to the flow exceeding 60 degrees the data for the grooves normal to the flow apply, while for grooves inclined between 0 degrees (parallel to the flow) and 60 degrees a method for obtaining the maximum increment is suggested based on the use of ESDU 75031 to predict the increments due to the forward- and rearward- facing steps together with an appropriate skin friction allowance.
Description
ESDU 75028 gives curves, derived from a correlation of experimental data, that enable the drag increment to be predicted due to a groove of planform aspect ratio greater than 8 normal to the flow. For grooves inclined at angles to the flow exceeding 60 degrees the data for the grooves normal to the flow apply, while for grooves inclined between 0 degrees (parallel to the flow) and 60 degrees a method for obtaining the maximum increment is suggested based on the use of ESDU 75031 to predict the increments due to the forward- and rearward- facing steps together with an appropriate skin friction allowance.

Suppliers

Company
Product
Description
Supplier Links
Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds. - 75028 - IHS ESDU
London, United Kingdom
Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds.
75028
Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds. 75028
ESDU 75028 gives curves, derived from a correlation of experimental data, that enable the drag increment to be predicted due to a groove of planform aspect ratio greater than 8 normal to the flow. For grooves inclined at angles to the flow exceeding 60 degrees the data for the grooves normal to the flow apply, while for grooves inclined between 0 degrees (parallel to the flow) and 60 degrees a method for obtaining the maximum increment is suggested based on the use of ESDU 75031 to predict the increments due to the forward- and rearward- facing steps together with an appropriate skin friction allowance.

ESDU 75028 gives curves, derived from a correlation of experimental data, that enable the drag increment to be predicted due to a groove of planform aspect ratio greater than 8 normal to the flow. For grooves inclined at angles to the flow exceeding 60 degrees the data for the grooves normal to the flow apply, while for grooves inclined between 0 degrees (parallel to the flow) and 60 degrees a method for obtaining the maximum increment is suggested based on the use of ESDU 75031 to predict the increments due to the forward- and rearward- facing steps together with an appropriate skin friction allowance.

Buy Now

Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 75028
Product Name Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds.
Unlock Full Specs
to access all available technical data

Similar Products