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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Memorandum Report
Two-dimensional wind-tunnel investigation of two NACA low-drag airfoil sections equipped with slotted flaps and a plain NACA low-drag airfoil section for XF6U-l airplane

Two-dimensional wind-tunnel investigation of two NACA low-drag airfoil sections equipped with slotted flaps and a plain NACA low-drag airfoil section for XF6U-l airplane

Date: January 1, 1946
Creator: Rice, Fred J , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical investigation of the stability of an F8F dropping model with automatic stabilization

Analytical investigation of the stability of an F8F dropping model with automatic stabilization

Date: December 1, 1945
Creator: Cohen, Doris
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section

Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section

Date: December 1, 1945
Creator: Cahill, Jones F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed wind-tunnel tests of a twin-fuselage pursuit airplane

High-speed wind-tunnel tests of a twin-fuselage pursuit airplane

Date: April 24, 1946
Creator: Tkac, Victor B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of Mach number on the aerodynamic characteristics of a single-engine pursuit airplane as determined from tests of a 1/3-scale model

The effect of Mach number on the aerodynamic characteristics of a single-engine pursuit airplane as determined from tests of a 1/3-scale model

Date: May 3, 1945
Creator: Jessen, Henry
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes

Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes

Date: April 23, 1943
Creator: Erickson, Albert L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An estimate of the effect of engine supercharging on the take-off thrust of a typical helicopter at different altitudes and temperatures

An estimate of the effect of engine supercharging on the take-off thrust of a typical helicopter at different altitudes and temperatures

Date: March 1, 1945
Creator: Voglewede, T J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Efficiency of a radial-flow exhaust-gas turbosupercharger turbine with a 12.75-inch tip diameter

Efficiency of a radial-flow exhaust-gas turbosupercharger turbine with a 12.75-inch tip diameter

Date: July 1, 1946
Creator: Gabriel, David S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Determination of air-consumption parameters for two radial aircraft engines

Determination of air-consumption parameters for two radial aircraft engines

Date: August 1, 1945
Creator: Howes, William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight tests of the Sikorsky HNS-1 (Army YR-4B) helicopter II : hovering and vertical-flight performance with the original and an alternate set of main-rotor blades, including a comparison with hovering performance theory

Flight tests of the Sikorsky HNS-1 (Army YR-4B) helicopter II : hovering and vertical-flight performance with the original and an alternate set of main-rotor blades, including a comparison with hovering performance theory

Date: April 1, 1945
Creator: Gessow, Alfred
Description: None
Contributing Partner: UNT Libraries Government Documents Department