The problem of time response of pressure gaging systems used with low density flows has been discussed in Ref ]4, and the effect of outgassing on pressure magnitudes was indicated in the same reference. Briefly, gases or vapors adhering to the internal walls of the pressure gaging system behave like gas sources and produce a pressure rise in the gage system which has no relation to the external flow. The effect can also occur in the reverse direction, with "in-gassing" or the action of an effective sink in the gage system as gases entering through the probe orifice are adsorbed to the walls. For given surface conditions, the magnitude of the pressure error to be expected due to out-gassing depends on the dimensions of the probe system. In t...
An investigation was conducted at Mach numbers of 1.41, 1.83, and 2.20 to determine the effects of p...
It is shown that adequate means are available for calculating inviscid direct and induced pressures ...
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...
An investigation of the behavior of flat-faced, impact-pressure probes with a range of orificeto-pro...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
For the determination of the flow velocity one is accustomed to measure the impact pressure, i.e., t...
An experimental investigation was undertaken at a nominal Mach number of 5.6 in the GALCIT Hypersoni...
The goal of this paper is to describe the idea of measuring a supersonic gas flow within low-pressur...
The removal of gas material through a capillary opening in a surface is analyzed. The gas, from whic...
Measurements of the steady pressure in a fluid flow may be required to determine other thermodynamic...
Measurements of the steady pressure in a fluid flow may be required to determine other thermodynamic...
The test probe was designed to measure free-stream Mach number and could be incorporated into a conv...
An investigation was conducted at Mach numbers of 1.41, 1.83, and 2.20 to determine the effects of p...
It is shown that adequate means are available for calculating inviscid direct and induced pressures ...
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...
An investigation of the behavior of flat-faced, impact-pressure probes with a range of orificeto-pro...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
For the determination of the flow velocity one is accustomed to measure the impact pressure, i.e., t...
An experimental investigation was undertaken at a nominal Mach number of 5.6 in the GALCIT Hypersoni...
The goal of this paper is to describe the idea of measuring a supersonic gas flow within low-pressur...
The removal of gas material through a capillary opening in a surface is analyzed. The gas, from whic...
Measurements of the steady pressure in a fluid flow may be required to determine other thermodynamic...
Measurements of the steady pressure in a fluid flow may be required to determine other thermodynamic...
The test probe was designed to measure free-stream Mach number and could be incorporated into a conv...
An investigation was conducted at Mach numbers of 1.41, 1.83, and 2.20 to determine the effects of p...
It is shown that adequate means are available for calculating inviscid direct and induced pressures ...
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...