Title of article
Wind Tunnel Tests of a Shrouded Aircraft Inlet
Author/Authors
Murphy، نويسنده , , D. M.; Schein، نويسنده , , M. E، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 1998
Pages
7
From page
33
To page
39
Abstract
We describe tests of a shrouded aerosol inlet for a high-altitude jet
aircraft. Both the lip of the inlet and the shroud are NACA (National Committee for
Aeronautics, now known as NASA, or National Aeronautics and Space Administration)
airfoils. Wind tunnel tests show a smooth growth of the boundary layer in the
inlet, with an undisturbed core more than 1 m back from the entrance. The shroud
makes the inlet performance insensitive to angle of attack. Aerosol transmission
tests showed accurate sampling, although the Stokes numbers accessible in the wind
tunnel were less than 0.2
Journal title
Aerosol Science and Technology
Serial Year
1998
Journal title
Aerosol Science and Technology
Record number
430444
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