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 Collection: National Advisory Committee for Aeronautics Collection
High mach number, low-cowl-drag, external- compression inlet with subsonic dump diffuser

High mach number, low-cowl-drag, external- compression inlet with subsonic dump diffuser

Date: May 12, 1958
Creator: Connors, J. F. & Flaherty, R. J.
Description: Low cowl drag, external compression inlet with subsonic dump diffuser for high Mach number application.
Contributing Partner: UNT Libraries Government Documents Department
High-altitude performance of J71-A-11 turbojet engine and its components using JP-4 and gaseous-hydrogen fuels

High-altitude performance of J71-A-11 turbojet engine and its components using JP-4 and gaseous-hydrogen fuels

Date: May 29, 1957
Creator: Saari, M. J. & Smith, I. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Influence of boric oxide deposition on turbojet-engine operation

Influence of boric oxide deposition on turbojet-engine operation

Date: February 15, 1957
Creator: Burley, R. R.; Useller, J. W. & Velie, W. W.
Description: Influence of boric oxide deposition on turbojet engine operation.
Contributing Partner: UNT Libraries Government Documents Department
Interference effects of fuselage-stored missiles on inlet duct model of an interceptor-type aircraft at Mach numbers 1.5 to 1.9

Interference effects of fuselage-stored missiles on inlet duct model of an interceptor-type aircraft at Mach numbers 1.5 to 1.9

Date: April 24, 1957
Creator: Davis, O. H. & Piercy, T. G.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Interpretation of boundary-layer pressure-rake data in flow with a detached shock

Interpretation of boundary-layer pressure-rake data in flow with a detached shock

Date: August 24, 1950
Creator: Luidens, R. W. & Madden, R. T.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Influence of Combustion-chamber Length on Afterburner Performance

Influence of Combustion-chamber Length on Afterburner Performance

Date: August 27, 1954
Creator: Braithwaite, W. M.; Rudey, C. J. & Useller, J. W.
Description: Combustion-chamber length influence on turbojet engine afterburner performance.
Contributing Partner: UNT Libraries Government Documents Department
De-icing Effectiveness of External Electric Heaters for Propeller Blades

De-icing Effectiveness of External Electric Heaters for Propeller Blades

Date: February 1, 1948
Creator: Lewis, J. P.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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
Organophosphorus compounds in rocket-engine applications

Organophosphorus compounds in rocket-engine applications

Date: April 2, 1954
Creator: Hennings, G. & Ladanyi, D. J.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Performance at high temperatures and pressures of an annular turbojet combustor having articulated liner walls

Performance at high temperatures and pressures of an annular turbojet combustor having articulated liner walls

Date: May 10, 1957
Creator: McCafferty, Richard J.; Wear, Jerrold D. & Cook, William P.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of control signals for variable ramps of twin-duct side inlets

Investigation of control signals for variable ramps of twin-duct side inlets

Date: January 16, 1958
Creator: Beheim, M. A. & Yeager, R. A.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of Effect of Number and Width of Annular Flameholder Gutters on Afterburner Performance

Investigation of Effect of Number and Width of Annular Flameholder Gutters on Afterburner Performance

Date: June 3, 1954
Creator: Bryant, L. & Henzel, J. G., Jr.
Description: Annular flame-holder gutters and afterburner combustion efficiency.
Contributing Partner: UNT Libraries Government Documents Department
Investigation of high-angle-of-attack performance of a 14 deg ramp-type inlet in various circumferential body locations, Mach number range 1.5 to 2.0

Investigation of high-angle-of-attack performance of a 14 deg ramp-type inlet in various circumferential body locations, Mach number range 1.5 to 2.0

Date: June 26, 1957
Creator: Chiccine, B. G. & Mitchell, G. A.
Description: Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at supersonic free stream.
Contributing Partner: UNT Libraries Government Documents Department
Investigation of Rotating-Stall Limits in a Supersonic Turbofan Engine

Investigation of Rotating-Stall Limits in a Supersonic Turbofan Engine

Date: October 3, 1957
Creator: Dugan, J. F.
Description: Rotating-stall limits in supersonic turbofan engine.
Contributing Partner: UNT Libraries Government Documents Department
Investigation of the air-flow-regulation characteristics of a translating-spike inlet with two oblique shocks from Mach 1.6 to 2.0

Investigation of the air-flow-regulation characteristics of a translating-spike inlet with two oblique shocks from Mach 1.6 to 2.0

Date: July 24, 1956
Creator: Nettles, J. C.
Description: Translating spike inlet air flow regulation characteristics from transonic to supersonic speeds at zero angle of attack.
Contributing Partner: UNT Libraries Government Documents Department