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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Research Memorandums
 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
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
Off-design performance of divergent ejectors

Off-design performance of divergent ejectors

Date: September 30, 1958
Creator: Beheim, Milton A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8

Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8

Date: September 30, 1958
Creator: Martz, C William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination

Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination

Date: September 30, 1958
Creator: Baker, Louis, Jr & Steffen, Fred W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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