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 Collection: National Advisory Committee for Aeronautics Collection
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
Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine

Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine

Date: March 10, 1954
Creator: Meyer, C. L. & Welna, H. J.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigations of slot configurations for film-cooled turbine blades by flow visualization methods

Investigations of slot configurations for film-cooled turbine blades by flow visualization methods

Date: October 10, 1950
Creator: Eckert, E. R. G.; Jackson, T. W. & Francisco, A. C.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Lateral-control Characteristics and Dihedral Effect of a Wingbody Combination With a Variable-incidence Triangular Wing and Wing-tip Ailerons at a Mach Number of 1.52

Lateral-control Characteristics and Dihedral Effect of a Wingbody Combination With a Variable-incidence Triangular Wing and Wing-tip Ailerons at a Mach Number of 1.52

Date: January 10, 1951
Creator: Dennis, D. H. & Scherrer, R.
Description: Aileron effectiveness & dihedral effect of wing- body combination with variable-incidence wing & half-delta controls at wing tips.
Contributing Partner: UNT Libraries Government Documents Department
Low-pressure performance of a tubular combustor with gaseous hydrogen

Low-pressure performance of a tubular combustor with gaseous hydrogen

Date: May 9, 1955
Creator: Hlavin, V. F.; Jonash, E. R. & Smith, A. L.
Description: Combustion performance characteristics of gaseous hydrogen fuel in single tubular turbojet combustor.
Contributing Partner: UNT Libraries Government Documents Department
A low-pressure-loss short afterburner for sea-level thrust augmentation

A low-pressure-loss short afterburner for sea-level thrust augmentation

Date: June 7, 1955
Creator: Burley, R. R.; Ciepluch, C. C. & Velie, W. W.
Description: Low-pressure-loss short afterburner design for sea level thrust augmentation of axial flow turbojet engine.
Contributing Partner: UNT Libraries Government Documents Department
Liquid Hydrogen as a Jet Fuel for High-altitude Aircraft

Liquid Hydrogen as a Jet Fuel for High-altitude Aircraft

Date: April 15, 1955
Creator: Hall, E. W. & Silverstein, A.
Description: Liquid hydrogen as jet fuel for high-altitude aircraft.
Contributing Partner: UNT Libraries Government Documents Department
Some effects of aeroelasticity on the rolling effectiveness of a 10-percent-scale model of the mc donnell f-101a airplane wing at mach numbers from 0.5 to 1.2

Some effects of aeroelasticity on the rolling effectiveness of a 10-percent-scale model of the mc donnell f-101a airplane wing at mach numbers from 0.5 to 1.2

Date: January 1, 1955
Creator: English, R. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Simulated Flight Investigation of Scaled-speed Elastic Sweptwing Bomber and Fighter Models Coupled Wing Tip to Wing Tip

Simulated Flight Investigation of Scaled-speed Elastic Sweptwing Bomber and Fighter Models Coupled Wing Tip to Wing Tip

Date: February 14, 1956
Creator: Thompson, R. F.
Description: Simulated flight tests of elastic swept-wing bomber and fighter model coupled wing tip to wing tip.
Contributing Partner: UNT Libraries Government Documents Department
Some effects of flow spoilers and of aerodynamic balance on the oscillating hinge moments for a swept fin-rudder combination in a transonic wind tunnel

Some effects of flow spoilers and of aerodynamic balance on the oscillating hinge moments for a swept fin-rudder combination in a transonic wind tunnel

Date: May 28, 1958
Creator: Gibson, F. W.; Herr, R. W. & Osborne, R. S.
Description: Flow spoiler and aerodynamic balance effects on oscillating hinge moments for swept fin-rudder combination in transonic wind tunnel.
Contributing Partner: UNT Libraries Government Documents Department