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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Research Memorandums
 Collection: Technical Report Archive and Image Library
Status of spin research for recent airplane designs

Status of spin research for recent airplane designs

Date: August 16, 1957
Creator: Neilhouse, Anshal I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat-exchanger-core weights for use with hydrogen expansion turbine

Heat-exchanger-core weights for use with hydrogen expansion turbine

Date: October 3, 1957
Creator: Reynolds, Thaine W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flutter and divergence of rectangular wings of very low aspect ratio

Flutter and divergence of rectangular wings of very low aspect ratio

Date: June 28, 1957
Creator: Fralich, Robert W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of string-support interference on the drag of an olgive-cylinder body with and without a boatail at 0.6 to 1.4 Mach number

Effects of string-support interference on the drag of an olgive-cylinder body with and without a boatail at 0.6 to 1.4 Mach number

Date: December 3, 1957
Creator: Lee, George
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections

The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections

Date: August 16, 1957
Creator: Westphal, Willard R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of wind tunnels to predict flight buffet loads

The use of wind tunnels to predict flight buffet loads

Date: June 10, 1957
Creator: Davis, Don D , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94

Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94

Date: August 12, 1957
Creator: Polhamus, Edward C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some properties of wing and half-body arrangements at supersonic speeds

Some properties of wing and half-body arrangements at supersonic speeds

Date: July 22, 1957
Creator: Migotsky, Eugene
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Exploratory investigation of the effect of wing slots and leading-edge slats on the longitudinal stability characteristics of a 45 degree sweptback wing-fuselage configuration

Exploratory investigation of the effect of wing slots and leading-edge slats on the longitudinal stability characteristics of a 45 degree sweptback wing-fuselage configuration

Date: February 8, 1957
Creator: Critzos, Chris C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model having double slotted flaps and spoilers

Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model having double slotted flaps and spoilers

Date: February 26, 1957
Creator: Croom, Delwin R
Description: None
Contributing Partner: UNT Libraries Government Documents Department