Effect of plug and shroud geometry variables on plug-nozzle performance at transonic speeds
Plug and shroud geometry variables on plug nozzle performance at transonic speeds
Berrier, B. L.↗
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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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Experimental investigation of a 10 deg conical turbojet plug nozzle with translating primary and secondary shrouds at Mach numbers from 0 to 2.0
Static tests of nozzle efficiency and pumping characteristics of conical turbojet plug nozzle with translating primary and secondary shrouds at Mach 0 to 2.0
Bresnahan, D. L.↗
Quiescent-air performance of a truncated turbojet plug nozzle with shroud and plug base flows from a common source
Performance characteristics of truncated, conical plug nozzle with cylindrical outer shroud
Johns, A. L.↗
Test plan for MARL experimental shroud test program
Test plan for vibration and acoustic tests on experimental shroud and payload
Kao, G. C.↗
Experimental results of varying the blade- shroud clearance in a 6.02-inch radial-inflow turbine
Experimental results of varying blade shroud clearance in 6.02 inch radial inflow turbine
Futral, S. M., Jr.↗
Effect of plug base contour on performance of a fully truncated plug nozzle with translating shroud
Effect of plug base contour on performance of fully truncated plug nozzle with translating shroud
Berrier, B. L.↗
Fabrication techniques for shrouded titanium impeller Final report, 29 Jun. 1967 - 30 Sep. 1969
Fabrication techniques for shrouded titanium impeller
Wolf, J. E.↗
Development of an SPS/DPS hydrogen shrouded cryogenic helium storage system Final report
SPS/DPS hydrogen shrouded cryogenic helium storage system
Bald, W. B.↗
Performance evaluation of a liquid-shrouded cryogenic storage system
Performance of cryogenic liquid shroud insulation for cryogenic fluid storage system
Mc Laughlan, P. B.↗
A theoretical and experimental model-study of the sound-induced vibration transmitted to a shroud-enclosed spacecraft Final report, 20 Jan. 1967 - 20 Jul. 1969
Theoretical and experimental model study of sound induced vibration transmitted to shroud enclosed spacecraft
Manning, J. E.↗
Composite powerplant and shroud therefor Patent
Shrouded composite propulsion system configuration
Escher, W. J. D.↗
Experimental evaluation of a honeycomb rotor shroud configuration to improve the stall margin of a 0.5 hub-tip ratio single-stage compressor. Volume 1 - Data and performance report
Experimental data and performance of honeycomb rotor shroud configuration to improve stall margin of 0.5 hub tip ratio single stage compressor
Oscarson, R. P.↗
Experimental evaluation of a honeycomb rotor shroud configuration to improve the stall margin of a 0.5 hub-tip ratio single-stage compressor. Volume 2 - Data supplement
Flow distribution data for solid and honeycomb rotor shrouds to improve stall margin of 0.5 hub tip ratio single stage compressor
Oscarson, R. P.↗
Prediction of the dynamic environment of spacecraft components. Part 2 - Acoustic and structural path transmission through two models of a shroud-enclosed spacecraft Final report
Acoustic and structural path transmission through shroud enclosed spacecraft
Greenspon, J. E.↗
Experimental investigation of heat-transfer characteristics of a film-cooled plug nozzle with translating shroud
Heat transfer characteristics of film cooled plug nozzle with translating shroud
Chenoweth, F. C.↗
Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel
Diffuser, shroud, and mass injection effects on starting and operating characteristics of Mach 5 free jet tunnel at low pressure ratios
Molloy, J. K.↗
Nonlinear response of gas-lubricated shrouded Rayleigh-step thrust pad
Quasi-static pressure characteristics of gas lubricated thrust bearing with shrouded Rayleigh step pads, solving nonlinear equation of motion
Cheng, C.↗
Computer simulation of temperatures on the Centaur standard shroud during heated jettison tests
A heating fixture for simulating the heating and environment encountered by the Centaur standard shroud (CSS) during its ascent through the earth's atmosphere is discussed. A computer program was developed to provide a means of determining the overall temperature profile of a free-skin model of the CSS during the heating portion of the heated jettison tests. The program treats the energy contribution of each lamp on the heater to various points on the CSS surface. The analytic model was verified by adapting the computer program to the configuration of the hardware used in a series of Intermediate Scale Tests performed on a 2.4 meters by 2.4 meters section of the CSS corrugated structure. A comparison of some predicted versus experimental results from these tests is presented.
Hemminger, J. A.↗