Computer calculation for determining compressible flow across radial face seals were compared with measured results obtained in a seal simulator rig at pressure ratios to 0.9 (ambient pressure/sealed pressure). In general, the measured and calculated leakages across the seal dam agreed within 3 percent. The resultant loss coefficient, dependent upon the pressure ratio, ranged from 0.47 to 0.68. The calculated pressures were within 2.5 N/cu um of the measured values
A detailed study was made of face and annular seals under conditions where boiling, i.e., phase chan...
A brief review of current annular seal theory and a discussion of the predicted effect on stiffness ...
The development of elastomeric face seals is imperative for NASA’s manned space flight program. Lack...
An analysis is presented for compressible fluid flow across shaft face seals and narrow slots. The a...
Analyses are presented for compressible fluid flow across shaft face seals with face deformation. Th...
A computer program is presented for compressible fluid flow with friction across face seals and thro...
The labyrinth seal is a non-contact annular type sealing device used to reduce the internal leakage ...
International audienceNon-contacting face seals rely on high pressures induced in a thin air-film be...
An analysis is presented for compressible fluid flow across shaft face seals and narrow slots. The a...
Computer program for analysis of compressible fluid flow across sealing dam consisting of two closel...
Computer program analyzes the flow /leakage/ across a sealing dam for the case of steady, laminar, s...
The basic equations are derived for compressible flow in a labyrinth seal. The flow is assumed to be...
The purposes of the computer tools for face seal analysis are new product optimization, existing sea...
A 36" diameter aspirating face seal for aircraft engine application has undergone extensive testing ...
The basic equations are derived for a two control volume model for compressible flow in a labyrinth ...
A detailed study was made of face and annular seals under conditions where boiling, i.e., phase chan...
A brief review of current annular seal theory and a discussion of the predicted effect on stiffness ...
The development of elastomeric face seals is imperative for NASA’s manned space flight program. Lack...
An analysis is presented for compressible fluid flow across shaft face seals and narrow slots. The a...
Analyses are presented for compressible fluid flow across shaft face seals with face deformation. Th...
A computer program is presented for compressible fluid flow with friction across face seals and thro...
The labyrinth seal is a non-contact annular type sealing device used to reduce the internal leakage ...
International audienceNon-contacting face seals rely on high pressures induced in a thin air-film be...
An analysis is presented for compressible fluid flow across shaft face seals and narrow slots. The a...
Computer program for analysis of compressible fluid flow across sealing dam consisting of two closel...
Computer program analyzes the flow /leakage/ across a sealing dam for the case of steady, laminar, s...
The basic equations are derived for compressible flow in a labyrinth seal. The flow is assumed to be...
The purposes of the computer tools for face seal analysis are new product optimization, existing sea...
A 36" diameter aspirating face seal for aircraft engine application has undergone extensive testing ...
The basic equations are derived for a two control volume model for compressible flow in a labyrinth ...
A detailed study was made of face and annular seals under conditions where boiling, i.e., phase chan...
A brief review of current annular seal theory and a discussion of the predicted effect on stiffness ...
The development of elastomeric face seals is imperative for NASA’s manned space flight program. Lack...