A method for predicting the performance of high reaction supersonic compressor blade sections.
Supersonic compressor blade sections performance prediction near maximum pressure ratio and efficiency by analyzing flow processes
Boxer, E.↗
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The computer-evaluation of wild-point rejection for telemetry data compressors.
Precompression automatic wild point rejection from sampled telemetry data for data compressors evaluated by digital computer simulation
Medlin, J. E.↗
Novel valve for reciprocating compressors - Concept
Thin ring valve for the inlets and exhausts of reciprocating compressors, and possibly for the inlets of internal combustion engines, encircles the cylinder and operates on the Bernoulli principle.
Wagner, C. E.↗
Integrated turbine-compressor provides air flow for cooling
Modified supersonic turbine cycle provides cooling air to surrounding structures. Simplified mechanical design assures correct balance of air flow, allows direct issue of cool air to the structure, and assists in matching turbine work output to work input required by the compressor.
Ferri, A.↗
TFE coating extends life of flexible metal compressor diaphragm
Tetrafluoroethylene /TFE/ aerosol sprayed onto entire surface of diaphragm acts as film lubricant and permits diaphragm to slide between upper and lower plates in a reciprocating compressor. Flexing occurs over an area rather than about a single line of action and operating life of diaphragm is more than quadrupled.
Gorland, S.↗
A study of discrete components of the noise spectrum of an axial compressor
Discrete components in noise frequency spectrum of axial compressor
Bazhenov, D. V.↗
Effect of the design of walls of the air intake duct of an axial compressor on the propagation of sound
Wall design effects of air intake duct in axial compressor on sound propagation
Bazhenov, D. V.↗
An application of theory to axial compressor noise. Appendix C - Bessel functions of the first kind - A table of values for orders to 179 and arguments to 211
Application of theory to axial compressor noise
Munch, C. L.↗
Effects of inlet-guide-vane configuration and relative blade velocity on noise from axial- flow compressors
Inlet-guide-vane configuration and relative blade velocity effects on noise reduction from axial flow compressors
Chestnutt, D.↗
Gas opacity measurements with a ballistic piston compressor
Ballistic piston compressor for opacity measurements of hot compressible gases
Hammond, G. L.↗
XB-70 compressor-noise reduction and propulsion-system performance for choked inlet flow
XB-70 compressor noise reduction and propulsion system performance for choked inlet flow
Putnam, T. W.↗
Measurements of the Van der Waals Na - lambda 5889 in He with a newly developed piston compressor light source
Measurements of Van der Waals Na 5889 A in He with piston compressor light source
Grindlay, J. E.↗
Design and development of a resonant piston compressor for hermetically sealed platforms
Resonant piston compressor for recirculation system of hermetically sealed platform
Curwen, P. W.↗
Single stage experimental evaluation of compressor blading with slots and vortex generators. Part 2 - Data and performance for stage 5 without slots or vortex generators
Comparison performance data of compressor blading without slots or vortex generators
Brent, J. A.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, part 6 Final report
Evaluation of outer case blowing or bleeding of single stage axial flow compressor
Koch, C. C.↗
Effect of Reynolds number on overall performance of a 6-inch radial bladed centrifugal compressor
Overall performance of centrifugal compressor over range of inlet pressures and corresponding Reynolds number
Ball, C. L.↗
Single stage experimental evaluation of compressor blading with slots and vortex generators. Part 1 - Analysis and design of stages 4 and 5
Analysis and design of compressor blading with slots and vortex generators
Brent, J. A.↗
The effect of inlet temperature distortion on the performance of a turbo-fan engine compressor system
Inlet temperature distortion effect on performance of turbofan engine compressor systems
Antl, R. J.↗