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 Decade: 1940-1949
 Year: 1947
 Collection: National Advisory Committee for Aeronautics Collection
The subsonic aerodynamic characteristics of two double-wedge airfoil sections suitable for supersonic flight

The subsonic aerodynamic characteristics of two double-wedge airfoil sections suitable for supersonic flight

Date: May 12, 1947
Creator: Solomon, Joseph & Henney, Floyd W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
: The linear perturbation theory of axially symmetric compressible flow with application to the effect of compressibility on the pressure coefficient at the surface of a body of revolution

: The linear perturbation theory of axially symmetric compressible flow with application to the effect of compressibility on the pressure coefficient at the surface of a body of revolution

Date: July 18, 1947
Creator: Herriot, John G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A study of several parameters controlling the trajectories of a supersonic antiaircraft missile powered with solid- or liquid-fuel rockets

A study of several parameters controlling the trajectories of a supersonic antiaircraft missile powered with solid- or liquid-fuel rockets

Date: April 24, 1947
Creator: Huntsberger, Ralph F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of perforated inlets for efficient supersonic diffusion

The use of perforated inlets for efficient supersonic diffusion

Date: June 25, 1947
Creator: Evvard, John C & Blakey, John W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A preliminary theoretical study of aerodynamic instability of a two-blade helicopter rotor

A preliminary theoretical study of aerodynamic instability of a two-blade helicopter rotor

Date: March 18, 1947
Creator: Coleman, Robert P & Stempin, Carl W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A summary report on the effects of Mach number on the span load distribution on wings of several models

A summary report on the effects of Mach number on the span load distribution on wings of several models

Date: July 15, 1947
Creator: Jessen, Henry, Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparative drag measurements at transonic speeds of an NACA 65-006 airfoil and a symmetrical circular-arc airfoil

Comparative drag measurements at transonic speeds of an NACA 65-006 airfoil and a symmetrical circular-arc airfoil

Date: March 6, 1947
Creator: Thompson, Jim Rogers & Marschner, Bernard W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions

The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions

Date: April 10, 1947
Creator: Allen, H Julian; Heaslet, Max A & Nitzberg, Gerald E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Measurements of the damping in roll of large-scale swept-forward and swept-back wings

Measurements of the damping in roll of large-scale swept-forward and swept-back wings

Date: July 30, 1947
Creator: Hunton, Lynn W & Dew, Joseph K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Free-flight investigation of control effectiveness of full-span 0.2-chord plain ailerons at high subsonic, transonic, and supersonic speeds to determine some effects of section thickness and wing sweepback

Free-flight investigation of control effectiveness of full-span 0.2-chord plain ailerons at high subsonic, transonic, and supersonic speeds to determine some effects of section thickness and wing sweepback

Date: May 29, 1947
Creator: Sandahl, Carl A & Marino, Alfred A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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