Gas turbine combustor Patent
Method for maintaining good performance in gas turbine during air flow distortion
Humenik, F. M.↗
Engineering topics
Norgren, C. T.
Publications and source records attributed to Norgren, C. T..
Gas turbine combustor insensitive to compressor outlet distortion
Short-length annular combustor for turbojet engines eliminates change of exit temperature profile. Individual scoops of full annular height control air distribution so that shifts in the radial velocity profile of air entering the combustor will not affect combustion process or alter exit temperature profile.
Humenik, F.↗
Dilution-jet mixing study for gas-turbine combustors
Dilution-jet mixing flow studies for gas turbine combustion chambers
Humenik, F. M.↗
Colloid thrustor beam analysis- design and operation of a suitable quadrupole mass filter
Colloid thrustor particle beam analysis - quadrupole mass filter design and operation
QUADRUPOLE↗
Experimental analysis of the exhaust beam from a colloid thrustor.
Exhaust beam from colloid thrustor investigated, using quadrupole mass filter
EXHAUST JET↗
Colloid propulsion method and apparatus Patent
Colloidal particle generator for electrostatic engine for propelling space vehicles
Norgren, C. T.↗
THRUST MEASUREMENTS OF COLLOIDAL PARTICLES AS AN INDICATION OF PARTICLE SIZE AND THRUSTOR OPERATION
Measurements of the thrust of a colloidal-particle electrostatic engine and their correlation to thrustor operation
PROPULSION SYSTEM PERFORMANCE↗
Thrust measurements of colloidal particles as an indication of particle size and thrustor operation
Thrust measurements of colloidal particles as indication of particle size & thrustor operation
THRUSTOR↗
ONBOARD COLLOIDAL PARTICLE GENERATOR FOR ELECTROSTATIC ENGINES
Colloidal particle generator for electrostatic rocket engine using a convergent-divergent nozzle
CONVERGENT-DIVERGENT NOZZLE↗
ONBOARD COLLOIDAL PARTICLE GENERATOR FOR ELECTROSTATIC ENGINES
Onboard colloidal particle generator for electrostatic engines
ELECTROSTATIC PROPULSION↗
ONBOARD COLLOIDAL PARTICLE GENERATOR FOR ELECTROSTATIC ENGINES
Spacecraft colloidal generator for electrostatic propulsion
SPACECRAFT PROPULSION↗
Onboard colloidal particle generator for electrostatic engines
Explore the source record for details and available documents.
Norgren, C. T.↗
Design and performance of an experimental annular turbojet combustor with high-velocity- air admission through one wall
Experimental annular turbojet combustor with high velocity air admission through one wall
ANNULAR FLOW↗
Performance at simulated high altitudes of a prevaporizing annular turbojet combustor having low pressure loss
Performance characteristics at simulated high altitudes of prevaporizing annular turbojet combustor with low pressure loss
COMBUSTOR↗
COMBUSTION PERFORMANCE OF TWO EXPERIMENTAL TURBOJET ANNULAR COMBUSTORS AT CONDITIONS SIMULATING HIGH-ALTITUDE SUPERSONIC FLIGHT
Performance of experimental annular turbojet combustors at simulated high altitude supersonic flight conditions
COMBUSTOR↗
EFFECT OF FUEL INJECTORS AND LINER DESIGN ON PERFORMANCE OF AN ANNULAR TURBOJET COMBUSTOR WITH VAPOR FUEL
Effect of fuel injector and liner design on performance of turbojet combustor with vapor fuel
COMBUSTOR↗