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 Collection: National Advisory Committee for Aeronautics Collection
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