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 Decade: 1940-1949
 Serial/Series Title: NACA Research Memorandums
 Collection: National Advisory Committee for Aeronautics Collection
The effects of fuel sloshing on the lateral stability of a free-flying airplane model

The effects of fuel sloshing on the lateral stability of a free-flying airplane model

Date: June 29, 1948
Creator: Smith, Charles C., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of a variable Mach number supersonic tunnel with nonintersecting characteristics

Investigation of a variable Mach number supersonic tunnel with nonintersecting characteristics

Date: November 15, 1948
Creator: Evvard, John C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers III : normal-shock diffuser

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers III : normal-shock diffuser

Date: December 22, 1948
Creator: Schroeder, Albert H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of two all-movable wings tested in the presence of a fuselage at a Mach number of 1.9

Aerodynamic characteristics of two all-movable wings tested in the presence of a fuselage at a Mach number of 1.9

Date: October 28, 1948
Creator: Conner, D William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Determination of average heat-transfer coefficients for a cascade of symmetrical impulse turbine blades I : heat transfer from blades to cold air

Determination of average heat-transfer coefficients for a cascade of symmetrical impulse turbine blades I : heat transfer from blades to cold air

Date: November 10, 1948
Creator: Meyer, Gene L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of effects of movable exhaust-nozzle plug on operational performance of 20-inch ram jet

Investigation of effects of movable exhaust-nozzle plug on operational performance of 20-inch ram jet

Date: July 27, 1948
Creator: Sterbentz, William H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of horizontal tails II : unswept and 35 degree swept-back plan forms of aspect ratio 4.5

Wind-tunnel investigation of horizontal tails II : unswept and 35 degree swept-back plan forms of aspect ratio 4.5

Date: June 3, 1948
Creator: Dods, Jules B , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Method for stress analysis of a swept propeller

Method for stress analysis of a swept propeller

Date: September 27, 1948
Creator: Whitcomb, Richard T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of the propeller slipstream on the characteristics of submerged inlets

The effect of the propeller slipstream on the characteristics of submerged inlets

Date: September 9, 1949
Creator: Delany, Noel K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers I : shock diffuser with triple-shock projecting cone

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers I : shock diffuser with triple-shock projecting cone

Date: September 15, 1948
Creator: Connors, J F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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