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 Collection: National Advisory Committee for Aeronautics Collection
Performance of an All-internal Conical Compression Inlet With Annular Throat Bleed at Mach Number 5.0

Performance of an All-internal Conical Compression Inlet With Annular Throat Bleed at Mach Number 5.0

Date: August 6, 1958
Creator: Obery, L. J. & Stitt, L. E.
Description: Internal compression inlet with throat bleed-off at hypersonic flow.
Contributing Partner: UNT Libraries Government Documents Department
Performance of an isentropic, all-internal- contraction, axisymmetric inlet designed for mach 2.50

Performance of an isentropic, all-internal- contraction, axisymmetric inlet designed for mach 2.50

Date: September 15, 1958
Creator: Anderson, B. H. & Bowditch, D. N.
Description: Performance of internal contraction, axisymmetric inlet with isentropic compression surfaces on cowl and centerbody at Mach 2.0 to 2.7.
Contributing Partner: UNT Libraries Government Documents Department
Performance of JP-4 fuel with fluorine- oxygen mixtures in 1000-pound-thrust rocket engines

Performance of JP-4 fuel with fluorine- oxygen mixtures in 1000-pound-thrust rocket engines

Date: June 11, 1958
Creator: Douglass, H. W. & Nored, D. L.
Description: Fluorine-liquid oxygen mixture and injector design effects on JP-4 jet fuel performance in rocket engines.
Contributing Partner: UNT Libraries Government Documents Department
Performance of five short multielement turbojet combustors for hydrogen fuel in quarter-annulus duct

Performance of five short multielement turbojet combustors for hydrogen fuel in quarter-annulus duct

Date: July 22, 1958
Creator: Jones, R. E. & Rayle, W. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Performance of Isentropic Nose Inlets at Mach Number of 5.6

Performance of Isentropic Nose Inlets at Mach Number of 5.6

Date: May 6, 1954
Creator: Bernstein, H. & Haefeli, R. C.
Description: Isentropic nose inlet performance at mach 5.6.
Contributing Partner: UNT Libraries Government Documents Department
Performance of several half-conical side inlets at supersonic and subsonic speeds

Performance of several half-conical side inlets at supersonic and subsonic speeds

Date: February 1, 1956
Creator: Cubbison, R. W.; Flaherty, R. J. & Stitt, L. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Performance of twin-duct variable-geometry side inlets at mach numbers of 1.5 to 2.0

Performance of twin-duct variable-geometry side inlets at mach numbers of 1.5 to 2.0

Date: January 21, 1957
Creator: Beheim, M. A.; Klann, J. L. & Yeager, R. A.
Description: Supersonic wind tunnel test of twin-duct variable geometry side inlets.
Contributing Partner: UNT Libraries Government Documents Department
Performance of Pentaborane, Pentaborane - Jp-4 Fuel Mixtures, and Trimethylborate Azeotrope Fuel in a Full-scale Turbojet Engine

Performance of Pentaborane, Pentaborane - Jp-4 Fuel Mixtures, and Trimethylborate Azeotrope Fuel in a Full-scale Turbojet Engine

Date: November 20, 1956
Creator: Breitwieser, R. & Useller, J. W.
Description: Full scale turbojet engine testing of fuels - pentaborane-jp-4 mixtures and trimethylborate azeotrope performance.
Contributing Partner: UNT Libraries Government Documents Department
Performance of Variable Two-dimensional Inlet Designed for Engine-inlet Matching. I - Performance at Design Mach Number of 3.07

Performance of Variable Two-dimensional Inlet Designed for Engine-inlet Matching. I - Performance at Design Mach Number of 3.07

Date: November 20, 1956
Creator: Beheim, M. A. & Gertsma, L. W.
Description: Supersonic performance of variable two-dimensional inlets designed for engine-inlet matching.
Contributing Partner: UNT Libraries Government Documents Department
High altitude performance investigation of J65-B-3 turbojet engine with both JP-4 and gaseous hydrogen fuels

High altitude performance investigation of J65-B-3 turbojet engine with both JP-4 and gaseous hydrogen fuels

Date: April 2, 1957
Creator: Kaufman, H. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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