Compressor and turbine matching
Compressor and gas turbine engine matching - power turbine, turbojet, and turboprop engines
AXIAL FLOW COMPRESSOR↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Rotor-stator interaction noise studies of a single-stage axial-flow research compressor
Far field noise propagation of rotor-stator interaction in single stage axial flow research compressor
STATOR BLADE↗
Use of a single turning vane to eliminate flow separation in a space-limited 90 deg intake elbow of an axial-flow compressor
Single turning vane for elimination of flow separation in intake elbow of axial flow compressor
ELBOW↗
Optimized turning-vane design for an intake elbow of an axial-flow compressor
Elbow turning vane design for high recovery and Uniform distribution at exit of 90 deg intake elbow of axial flow compressor
ELBOW↗
Experimental noise studies of inlet-guide- vane-rotor-stator interactions for a single- stage axial-flow compressor
Noise generation in axial flow compressors - acoustic data in form of noise radiation patterns from inlet-guide-vane-rotor-stator interactions
ROTOR BLADE↗
Design and fabrication of a high-performance Brayton-cycle compressor research package Final report
Advanced aerodynamic design and specifications of high efficiency Brayton cycle compressor for monatomic gas operation
COMPRESSOR↗
Development of compressor end seals stator interstage seals, and stator pivot seals in air breathing propulsion systems Semiannual report no. 1, 29 Jun. - 31 Dec. 1965
Seal concepts evaluation for compressor end seals, stator interchange seals, and stator pivot seals in air breathing propulsion system
SEALING↗
Brayton cycle 3.2-inch radial compressor performance evaluation
Brayton cycle 3.2 inch radial compressor performance evaluation over wide range of Reynolds numbers
COMPRESSOR EFFICIENCY↗
Methods of predicting the effect of shear flows on the outlet angle in axial compressor cascades.
Outlet angle in axial compressor cascades, accounting for effect of shear flows, Bernoulli surface rotation and flow separation
FLOW SEPARATION↗
The flow induction process of compressors designed to accept supersonic inflow velocity.
Supersonic compressor flow induction process as affected by Mach number, cone angle, rotational speed and blade angle
MACH NUMBER↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part I - Design of rotor and bleeding and blowing configurations
Rotor design to evaluate outer case blowing or bleeding of single stage axial flow compressor
BLOWING↗
Turbine research package for research and development of high performance axial flow turbine-compressor Final report
Turbine research package for research and development of high performance axial flow turbine compressor
BRAYTON CYCLE↗
Test of a cracked compressor blade repaired by electron beam welding
Feasibility of electron beam welding for repairing cracked compressor blades
COMPRESSOR BLADE↗
Contribution of downstream stator to the interaction noise of a single-stage axial-flow compressor
Downstream stator contribution to interaction noise of single-stage axial flow compressor
NOISE REDUCTION↗
Compressor Research Package for Research and Development of High Performance Axial-flow Turbomachinery Final Report
Compressor research package to provide aerodynamic performance data for Brayton-cycle axial flow turbomachinery
AXIAL FLOW COMPRESSOR↗
Single stage experimental evaluation of high Mach number compressor rotor blading. Part I - Design of rotor blading
Axial-flow medium aspect ratio compressor rotor blade rows designed to evaluate use of blade camberline shape to minimize blade element losses at high transonic speed
AXIAL FLOW COMPRESSOR↗
Development of compressor end seals, stator interstage seals, and stator pivot seals in advanced air breathing propulsion systems Semiannual report, 1 Jan. - 30 Jun. 1966
Design of compressor end, stator interface, and stator pivot seals for advanced air breathing engines
SEALING↗
Parametric study of advanced multistage axial-flow compressors
Axial flow compressor study to increase pressure ratio and reduce overall length
PRESSURE RATIO↗