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
Link To Document :
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