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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Advanced Restricted Report
 Collection: Technical Report Archive and Image Library
The effect of increased cooling surface on performance of aircraft-engine cylinders as shown by tests of the NACA cylinder

The effect of increased cooling surface on performance of aircraft-engine cylinders as shown by tests of the NACA cylinder

Date: July 1, 1944
Creator: Ellerbrock, Herman H , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculations of economy of 18-cylinder radial aircraft engine with exhaust-gas turbine geared to the crankshaft at cruising speed

Calculations of economy of 18-cylinder radial aircraft engine with exhaust-gas turbine geared to the crankshaft at cruising speed

Date: January 1, 1945
Creator: Zimmerman, Richard H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Correlation of exhaust-valve temperatures with engine operating conditions and valve design

Correlation of exhaust-valve temperatures with engine operating conditions and valve design

Date: January 1, 1945
Creator: Sanders, J C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel

Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel

Date: July 1, 1944
Creator: Ellerbrock, Herman H , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of spring tabs to elevator controls

Application of spring tabs to elevator controls

Date: October 1, 1944
Creator: Phillips, William H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight studies of the horizontal-tail loads experienced by a fighter airplane in abrupt maneuvers

Flight studies of the horizontal-tail loads experienced by a fighter airplane in abrupt maneuvers

Date: June 1, 1944
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation

Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation

Date: January 1, 1945
Creator: Houbolt, John C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The flow of a compressible fluid past a circular arc profile

The flow of a compressible fluid past a circular arc profile

Date: October 1, 1944
Creator: Kaplan, Carl
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The flow of a compressible fluid past a curved surface

The flow of a compressible fluid past a curved surface

Date: November 1, 1943
Creator: Kaplan, Carl
Description: None
Contributing Partner: UNT Libraries Government Documents Department
On the plane potential flow past a symmetrical lattice of arbitrary airfoils

On the plane potential flow past a symmetrical lattice of arbitrary airfoils

Date: January 1, 1944
Creator: Garrick, I E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Single-cylinder oil-control tests of porous chrome plated cylinder barrels for radial air-cooled engines

Single-cylinder oil-control tests of porous chrome plated cylinder barrels for radial air-cooled engines

Date: January 1, 1946
Creator: Swikert, Max
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel procedure for determination of critical stability and control characteristics of airplanes

Wind-tunnel procedure for determination of critical stability and control characteristics of airplanes

Date: April 1, 1944
Creator: Belsley, Steven E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of compressibility on two-dimensional tunnel-wall interference for a symmetrical airfoil

The effect of compressibility on two-dimensional tunnel-wall interference for a symmetrical airfoil

Date: January 1, 1943
Creator: Nitzberg, Gerald E
Description: Summary: The effective change in the velocity of flow past a wing section, caused by the presence of wind-tunnel walls, is known for potential flow. This theory is extended by investigation of the two-dimensional compressible flow past a thin Rankine Oval. It is shown that for a symmetrical section at zero angle of attack the velocity increment due to the tunnel walls in the incompressible case must be multiplied by the factor 1/1-M^2 to take account of compressibility effects. The Mach number, M, corresponds to conditions in the wind-tunnel test section with the model removed (p. 1.).
Contributing Partner: UNT Libraries Government Documents Department
An investigation of a thermal ice-prevention system for a C-46 cargo airplane III : description of thermal ice-prevention equipment for wings, empennage, and windshield

An investigation of a thermal ice-prevention system for a C-46 cargo airplane III : description of thermal ice-prevention equipment for wings, empennage, and windshield

Date: June 24, 1944
Creator: Spies, Ray J , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of a thermal ice-prevention system for a C-46 cargo airplane II : the design, construction, and preliminary tests of the exhaust-air heat exchanger

An investigation of a thermal ice-prevention system for a C-46 cargo airplane II : the design, construction, and preliminary tests of the exhaust-air heat exchanger

Date: June 20, 1944
Creator: Jackson, Richard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of a thermal ice-prevention system for a C-46 cargo airplane IV : results of flight tests in dry-air and natural-icing conditions

An investigation of a thermal ice-prevention system for a C-46 cargo airplane IV : results of flight tests in dry-air and natural-icing conditions

Date: July 7, 1944
Creator: Lewis, E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of a thermal ice-prevention system for a C-46 cargo airplane V : effect of thermal system on airplane cruise performance

An investigation of a thermal ice-prevention system for a C-46 cargo airplane V : effect of thermal system on airplane cruise performance

Date: January 13, 1945
Creator: Selna, James
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of a thermal ice-prevention system for a C-46 cargo airplane VI : dry-air performance of thermal system at several twin- and single-engine operating conditions at various altitudes

An investigation of a thermal ice-prevention system for a C-46 cargo airplane VI : dry-air performance of thermal system at several twin- and single-engine operating conditions at various altitudes

Date: May 1, 1945
Creator: Kees, Harold L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wall interference in a two-dimensional-flow wind tunnel with consideration of the effect of compressibility

Wall interference in a two-dimensional-flow wind tunnel with consideration of the effect of compressibility

Date: January 1, 1944
Creator: Vincenti, Walter G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Ultraviolet spectrochemical analysis for aromatics in aircraft fuels

Ultraviolet spectrochemical analysis for aromatics in aircraft fuels

Date: March 1, 1945
Creator: Cleaves, Alden P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of aircraft heaters XVIII : a design manual for exhaust gas and air heat exchangers

An investigation of aircraft heaters XVIII : a design manual for exhaust gas and air heat exchangers

Date: August 1945
Creator: Boelter, L. M. K.; Martinelli, R. C.; Romie, F. E. & Morrin, E. H.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Compressible potential flow with circulation about a circular cylinder

Compressible potential flow with circulation about a circular cylinder

Date: January 1, 1944
Creator: Heaslet, Max A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Nitrided-steel piston rings for engines of high specific power

Nitrided-steel piston rings for engines of high specific power

Date: January 1, 1945
Creator: Schmiedlin, Ralph F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A laboratory investigation of the icing characteristics of the Bendix-Stromberg carburetor model PD-12F5 with the Pratt and Whitney R-1830-C4 intermediate rear engine section

A laboratory investigation of the icing characteristics of the Bendix-Stromberg carburetor model PD-12F5 with the Pratt and Whitney R-1830-C4 intermediate rear engine section

Date: October 1, 1944
Creator: Essex, Henry A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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