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 Collection: National Advisory Committee for Aeronautics Collection
Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles

Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles

Date: February 11, 1952
Creator: Rousso, M. D. & Baughman, L. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of a 0.6 Hub-tip Radius-ratio Transonic Turbine Designed for Secondary-flow Study. Iii - Experimental Performance With Two Stator Configurations Designed to Eliminate Blade Wakes and Secondary-flow Effects and Conclusions From Entire Stator Investigation

Investigation of a 0.6 Hub-tip Radius-ratio Transonic Turbine Designed for Secondary-flow Study. Iii - Experimental Performance With Two Stator Configurations Designed to Eliminate Blade Wakes and Secondary-flow Effects and Conclusions From Entire Stator Investigation

Date: September 17, 1957
Creator: Moffitt, T. P.; Rohlik, H. E. & Wintucky, W. T.
Description: Hub-tip radius ratio transonic turbine for secondary flow - stator configurations designed to eliminate blade wakes and secondary-flow effects.
Contributing Partner: UNT Libraries Government Documents Department
Hydrogen for turbojet and ramjet powered flight

Hydrogen for turbojet and ramjet powered flight

Date: April 26, 1957
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Measurement and analysis of turbulent flow containing periodic flow fluctuations

Measurement and analysis of turbulent flow containing periodic flow fluctuations

Date: August 19, 1953
Creator: Mickelsen, W. R. & Laurence, J. C.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Low-temperature Chemical Starting of a 200-pound-thrust Jp-4 - Nitric Acid Rocket Engine Using a Three-fluid Propellant Valve

Low-temperature Chemical Starting of a 200-pound-thrust Jp-4 - Nitric Acid Rocket Engine Using a Three-fluid Propellant Valve

Date: June 30, 1955
Creator: Hennings, G. & Morrell, G.
Description: Low-temperature chemical starting of combined jp-4 nitric acid propellant for low-thrust rocket engine using three-fluid propellant valve.
Contributing Partner: UNT Libraries Government Documents Department
Nonuniform Burnup and Poisoning Effects in a Reactor and Validity of Uniform Approximation

Nonuniform Burnup and Poisoning Effects in a Reactor and Validity of Uniform Approximation

Date: March 9, 1953
Creator: Spooner, R. B.
Description: Burnup and poisoning in nuclear reactor core and validity of uniform approximation.
Contributing Partner: UNT Libraries Government Documents Department
Measurement of distortion in second experimental control rod for argonne naval reactor with constant transverse temperature gradient and uniform longitudinal temperature distribution

Measurement of distortion in second experimental control rod for argonne naval reactor with constant transverse temperature gradient and uniform longitudinal temperature distribution

Date: September 26, 1951
Creator: Lietzke, A. F. & Nagey, T. F.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Operation of an experimental air-cooled turbojet engine at turbine-inlet temperatures from 2200 R to 2935 R

Operation of an experimental air-cooled turbojet engine at turbine-inlet temperatures from 2200 R to 2935 R

Date: August 20, 1956
Creator: Cochran, R. P.; Dengler, R. P. & Esgar, J. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Off-Design Performance of Divergent Ejectors

Off-Design Performance of Divergent Ejectors

Date: September 30, 1958
Creator: Beheim, M. A.
Description: Off-design performance of divergent ejectors.
Contributing Partner: UNT Libraries Government Documents Department
Performance and operational characteristics of pentaborane fuel in 48-inch-diameter ram-jet engine

Performance and operational characteristics of pentaborane fuel in 48-inch-diameter ram-jet engine

Date: April 24, 1957
Creator: Farley, J. M.; Rayle, W. D. & Reilly, D. H., Jr.
Description: Combustion efficiency of pentaborane fuel in 48- inch diameter ramjet engine.
Contributing Partner: UNT Libraries Government Documents Department