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 Decade: 1940-1949
 Collection: National Advisory Committee for Aeronautics Collection
Stress and distortion measurements in a 45 degree swept box beam subjected to bending and to torsion

Stress and distortion measurements in a 45 degree swept box beam subjected to bending and to torsion

Date: March 1, 1948
Creator: Zender, George
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel tests and analysis of two 10-foot-diameter six-blade dual-rotating tractor propeller differing in pitch distribution

Wind-tunnel tests and analysis of two 10-foot-diameter six-blade dual-rotating tractor propeller differing in pitch distribution

Date: June 1, 1948
Creator: Gilman, Jean, Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line designed to produce a high critical Mach number

An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line designed to produce a high critical Mach number

Date: July 1, 1948
Creator: Loftin, Laurence K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Gust-tunnel tests to determine influence of airfoil section characteristics on gust-load factors

Gust-tunnel tests to determine influence of airfoil section characteristics on gust-load factors

Date: July 1, 1948
Creator: Pierce, Harold B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Recurrence formulas and differential equations for stress analysis of cambered box beams

Recurrence formulas and differential equations for stress analysis of cambered box beams

Date: October 1, 1947
Creator: Kempner, Joseph
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Low-speed static stability and damping-in-roll characteristics of some swept and unswept low-aspect-ratio wings

Low-speed static stability and damping-in-roll characteristics of some swept and unswept low-aspect-ratio wings

Date: October 1, 1947
Creator: Tosti, Louis P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Supersonic wave drag of nonlifting sweptback tapered wings with Mach lines behind the line of maximum thickness

Supersonic wave drag of nonlifting sweptback tapered wings with Mach lines behind the line of maximum thickness

Date: August 1, 1948
Creator: Margolis, Kenneth
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness

Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness

Date: September 1, 1948
Creator: Tucker, Warren A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing alone

Investigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing alone

Date: October 1, 1948
Creator: Hieser, Gerald
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of Reynolds number in turbulent-flow range on flame speeds of Bunsen-burner flames

Effect of Reynolds number in turbulent-flow range on flame speeds of Bunsen-burner flames

Date: September 1, 1948
Creator: Bollinger, Lowell M
Description: None
Contributing Partner: UNT Libraries Government Documents Department