COMBINED COMPRESSOR COOLANT INJECTION AND AFTERBURNING FOR TURBOJET THRUST AUGMENTATION
Combined compressor coolant injection and afterburning for turbojet engine thrust augmentation
AFTERBURNING↗
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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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CALCULATED PERFORMANCE OF A MERCURY-COMPRESSOR-JET POWERED AIRPLANE USING A NUCLEAR REACTOR AS AN ENERGY SOURCE
Calculated performance of a mercury-compressor- jet powered aircraft using nuclear reactor as energy source
JET AIRCRAFT↗
Compressor design requirements
Cycle analysis of turbojet and turboprop engines - axial flow compressor requirements for gas turbine engines
AXIAL FLOW COMPRESSOR↗
Compressor design system
Thermodynamic equations, solution, and experimental data for aerodynamic design of axial flow compressors
AERODYNAMICS↗
Compressor surge
Steady state characteristics, stalling, and surge in axial flow compressors
STEADY STATE↗
Three-dimensional compressor flow theory and real flow effects
Three-dimensional compressor flow theory and real flow effect
AXIAL FLOW COMPRESSOR↗
Effects of design and measurement errors on compressor performance
Design and measurement error effects on compressor performance
ERROR↗
Compressor and turbine matching
Compressor and gas turbine engine matching - power turbine, turbojet, and turboprop engines
AXIAL FLOW COMPRESSOR↗
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↗