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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Collection: National Advisory Committee for Aeronautics Collection
Performance of a Single Fuel-vaporizing Combustor With Six Injectors Adapted for Gaseous Hydrogen

Performance of a Single Fuel-vaporizing Combustor With Six Injectors Adapted for Gaseous Hydrogen

Date: November 30, 1959
Creator: Smith, A. L. & Wear, J. D.
Description: Single fuel-vaporizing combustor with injectors adapted for gaseous hydrogen.
Contributing Partner: UNT Libraries Government Documents Department
Some Research on the Lift and Stability of Wing-Body Combinations

Some Research on the Lift and Stability of Wing-Body Combinations

Date: July 2, 1959
Creator: Purser, Paul E. & Fields, E. M.
Description: The present paper summarizes and correlates broadly some of the research results applicable to fin-stabilized ammunition. The discussion and correlation are intended to be comprehensive, rather than detailed, in order to show general trends over the Mach number range up to 7.0. Some discussion of wings, bodies, and wing-body interference is presented, and a list of 179 papers containing further information is included. The present paper is intended to serve more as a bibliography and source of reference material than as a direct source of design information.
Contributing Partner: UNT Libraries Government Documents Department
Preliminary analysis of hydrogen-rich hypersonic ramjet operation

Preliminary analysis of hydrogen-rich hypersonic ramjet operation

Date: May 29, 1959
Creator: Breitwieser, R. & Morris, J. F.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical evaluation of the effects of an aerodynamic modification and of stability augmenters on the pitch behavior and probable pilot opinion of two current fighter airplanes

An analytical evaluation of the effects of an aerodynamic modification and of stability augmenters on the pitch behavior and probable pilot opinion of two current fighter airplanes

Date: April 21, 1959
Creator: Sadoff, Melvin & Stewart, John D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1.60 to 2.50

Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1.60 to 2.50

Date: April 15, 1959
Creator: Church, J. D.
Description: Wind tunnel testing of swept wing fighter aircraft model for determining drag and static longitudinal and lateral stability and control characteristics.
Contributing Partner: UNT Libraries Government Documents Department
Boundary-layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6

Boundary-layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6

Date: January 1, 1959
Creator: Bertram, M. H.
Description: Boundary layer displacement effects in air at mach 6.8 and 9.6.
Contributing Partner: UNT Libraries Government Documents Department
Forty-Fourth Annual Report of the National Advisory Committee for Aeronautics Administrative Report Including Technical Reports Nos. 1342 to 1392

Forty-Fourth Annual Report of the National Advisory Committee for Aeronautics Administrative Report Including Technical Reports Nos. 1342 to 1392

Date: January 1, 1959
Creator: unknown
Description: In accordance with act of Congress, approved March 3, 1915, as amended (U.S.C., title 50, .sw 151), which established the National Advisory Committee for Aeronautics, the Committee submits its Forty-fourth Annual Report for the fiscal year 1958. This is the Committee's final report to the Congress. The National Aeronautics and Space Act of 1958 (Public Law 85-568) provides in section 301 that the NACA "shall cease to exist" and "all functions, powers, duties, and obligations, and all real and personal property, personnel (other than members of the Committee), funds, and records of the NACA shall be transferred to the National Aeronautics and Space Administration. The aforesaid act provides that "this section shall take effect 90 days after the date of the enactment of this act, or on any earlier date on which the Administrator shall determining and announce by proclamation published in the Federal Register, that the Administration has been organized and is prepared to discharge the duties and exercise the power conferred upon it by this act." The Administrator, Hon. T. Keith Glennan has advised the Committee of his intention to issue such proclamation, effective October 1,1958.
Contributing Partner: UNT Libraries Government Documents Department
One-dimensional flows of an imperfect diatomic gas

One-dimensional flows of an imperfect diatomic gas

Date: January 1, 1959
Creator: unknown
Description: With the assumptions that Berthelot's equation of state accounts for molecular size and intermolecular force effects, and that changes in the vibrational heat capacities are given by a Planck term, expressions are developed for analyzing one-dimensional flows of a diatomic gas. The special cases of flow through normal and oblique shocks in free air at sea level are investigated. It is found that up to a Mach number 10 pressure ratio across a normal shock differs by less than 6 percent from its ideal gas value; whereas at Mach numbers above 4 the temperature rise is considerable below and hence the density rise is well above that predicted assuming ideal gas behavior. It is further shown that only the caloric imperfection in air has an appreciable effect on the pressures developed in the shock process considered. The effects of gaseous imperfections on oblique shock-flows are studied from the standpoint of their influence on the life and pressure drag of a flat plate operating at Mach numbers of 10 and 20. The influence is found to be small. (author).
Contributing Partner: UNT Libraries Government Documents Department
Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine

Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine

Date: September 30, 1958
Creator: Heidmann, M F & Baker, Louis, Jr
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
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