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 Collection: National Advisory Committee for Aeronautics Collection
Exploratory Investigation of Performance of Experimental Fuelrich Hydrogen Combustion System

Exploratory Investigation of Performance of Experimental Fuelrich Hydrogen Combustion System

Date: June 25, 1958
Creator: Grobman, J. S. & Smith, A. L.
Description: Exploratory investigation of performance characteristics of fuel-rich hydrogen combustor.
Contributing Partner: UNT Libraries Government Documents Department
Flight investigation of a liquid hydrogen fuel system

Flight investigation of a liquid hydrogen fuel system

Date: August 19, 1957
Creator: Acker, L. W.; Christenson, H. H.; Gough, W. V. & Mulholland, D. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Performance of an Inlet Having a Variable-angle Two-dimensional Compression Surface and a Fixed-geometry Subsonic Diffuser for Application to Reduced Engine Rotative Speeds- Mach Numbers 0.66, 1.5, 1.7, and 2.0

Performance of an Inlet Having a Variable-angle Two-dimensional Compression Surface and a Fixed-geometry Subsonic Diffuser for Application to Reduced Engine Rotative Speeds- Mach Numbers 0.66, 1.5, 1.7, and 2.0

Date: January 30, 1958
Creator: Allen, J. L.
Description: Air inlet for turbojet engines having variable angle two-dimensional compression surface and fixed-geometry subsonic diffuser.
Contributing Partner: UNT Libraries Government Documents Department
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