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 I 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
An investigation was conducted in the Langley 4- by 6-foot tunnel to determine the boundary-layer ch...
A model of a scramjet inlet was investigated experimentally in the hypersonic wind tunnel H2K of DLR...
Pressure distributions on three NACA 1-series inlets have been obtained in the Langley 16-Foot Trans...
We describe tests of a shrouded aerosol inlet for a high-altitude jet aircraft. Both the lip of the ...
Installation of the wing-root inlet was accomplished with no significant effects on the force charac...
Air inlets in some form are used on all commercial airliners today. The type of air inlet investigat...
A low-speed investigation has been conducted in the Langley two-dimensional low-turbulence tunnel to...
The supersonic free-flight wind tunnel is a facility at the Ames Laboratory of the NACA in which aer...
A low-speed investigation has been conducted in the Langley two-dtiensional low-turbulence tunnel to...
A novel inlet has been designed for selective sampling of gas and aerosol phases of volatile species...
This report covers the first part of an experimental investigation of NACA submerged inlets at four ...
Tests have been made by the National Advisory Committee for Aeronautics on the air flow in an open j...
A brief summary is made of the performance of a series of variable-geometry type scoop inlets invest...
An investigation was made in the NACA 5-foot vertical wind tunnel of a large variety of duct inlets ...
Abstract The NACA 633‐418 airfoil has been tested in the new Poul la Cour Wind Tunnel at the Technic...
An investigation was conducted in the Langley 4- by 6-foot tunnel to determine the boundary-layer ch...
A model of a scramjet inlet was investigated experimentally in the hypersonic wind tunnel H2K of DLR...
Pressure distributions on three NACA 1-series inlets have been obtained in the Langley 16-Foot Trans...
We describe tests of a shrouded aerosol inlet for a high-altitude jet aircraft. Both the lip of the ...
Installation of the wing-root inlet was accomplished with no significant effects on the force charac...
Air inlets in some form are used on all commercial airliners today. The type of air inlet investigat...
A low-speed investigation has been conducted in the Langley two-dimensional low-turbulence tunnel to...
The supersonic free-flight wind tunnel is a facility at the Ames Laboratory of the NACA in which aer...
A low-speed investigation has been conducted in the Langley two-dtiensional low-turbulence tunnel to...
A novel inlet has been designed for selective sampling of gas and aerosol phases of volatile species...
This report covers the first part of an experimental investigation of NACA submerged inlets at four ...
Tests have been made by the National Advisory Committee for Aeronautics on the air flow in an open j...
A brief summary is made of the performance of a series of variable-geometry type scoop inlets invest...
An investigation was made in the NACA 5-foot vertical wind tunnel of a large variety of duct inlets ...
Abstract The NACA 633‐418 airfoil has been tested in the new Poul la Cour Wind Tunnel at the Technic...
An investigation was conducted in the Langley 4- by 6-foot tunnel to determine the boundary-layer ch...
A model of a scramjet inlet was investigated experimentally in the hypersonic wind tunnel H2K of DLR...
Pressure distributions on three NACA 1-series inlets have been obtained in the Langley 16-Foot Trans...