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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Research Memorandums
 Collection: Technical Report Archive and Image Library
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
Meteorological problems associated with commercial turbojet-aircraft operation

Meteorological problems associated with commercial turbojet-aircraft operation

Date: June 21, 1955
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA investigation of fuels corresponding to specification AN-F-58 : results of studies in single combustors of J-33, J-34, J-35, and NENE turbojet engines

NACA investigation of fuels corresponding to specification AN-F-58 : results of studies in single combustors of J-33, J-34, J-35, and NENE turbojet engines

Date: November 16, 1945
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA Zero Power Reactor Facility Hazards Summary

NACA Zero Power Reactor Facility Hazards Summary

Date: June 24, 1957
Creator: unknown
Description: The Lewis Flight Propulsion Laboratory of the National Advisory Committee for Aeronautics proposes to build a zero power research reactor facility which will be located in the laboratory grounds near Clevelaurd, Ohio. The purpose of this report is to inform the Advisory Committee on Reactor Safeguards of the U. S. Atomic Energy Commission in regard to the design of the reactor facility, the cha,acteristics of the site, and the hazards of operation at this location, The purpose of this reactor is to perform critical experiments, to measure reactivity effects, to serve as a neutron source, and to serve as a training tool. The reactor facility is described. This is followed by a discussion of the nuclear characteristics and the control system. Site characteristics are then discussed followed by a discussion of the experiments which may be conducted in the facility. The potential hazards of the facility are then considered, particularly, the maximum credible accident. Finally, the administrative procedure is discussed.
Contributing Partner: UNT Libraries Government Documents Department
Preliminary study of use of nonstrategic metals for and application of cooling to blades of turbine of J35 turbojet engine

Preliminary study of use of nonstrategic metals for and application of cooling to blades of turbine of J35 turbojet engine

Date: November 17, 1948
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary survey of the aircraft fire problem

Preliminary survey of the aircraft fire problem

Date: May 21, 1948
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A restricted list of aircraft materials research projects

A restricted list of aircraft materials research projects

Date: May 4, 1948
Creator: unknown
Description: This report contains a selected list of Government sponsored research projects on related aircraft materials in effect during the calendar year 1947. Information is contained on titles, description, sponsoring and conducting agencies.
Contributing Partner: UNT Libraries Government Documents Department
Review of current and anticipated lubricant problems in turbojet engines

Review of current and anticipated lubricant problems in turbojet engines

Date: April 20, 1951
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Review of problems of conservation of strategic materials for turbine engines

Review of problems of conservation of strategic materials for turbine engines

Date: March 21, 1951
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Summary of Section Data on Trailing-Edge High-Lift Devices

Summary of Section Data on Trailing-Edge High-Lift Devices

Date: August 20, 1948
Creator: unknown
Description: A summary has been made of available data on the characteristics of airfoil sections with trailing-edge high-lift devices. Data for plain, split, and slotted flaps are collected and analyzed. The effects of each of the variables involved in the design of the various types of flap are examined and, in cases where sufficient data are given, optimum configurations are deduced. Wherever possible, the effects of airfoil section, Reynolds number, and leading-edge roughness are shown. For single and double slotted flaps, where a great mass of unrelated date are available, maximum lift coefficients of a large number of configurations are presented in tables.
Contributing Partner: UNT Libraries Government Documents Department