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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 high temperature of the cylinder head on the knocking tendency of an air-cooled engine cylinder

The effect of high temperature of the cylinder head on the knocking tendency of an air-cooled engine cylinder

Date: February 1, 1945
Creator: Peters, M D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Artificial running-in of piston rings

Artificial running-in of piston rings

Date: March 1, 1944
Creator: Machlin, E S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A cooling correlation of the Wright R-2600-8 engine showing the effect of water as an internal coolant

A cooling correlation of the Wright R-2600-8 engine showing the effect of water as an internal coolant

Date: February 1, 1945
Creator: Engelman, Helmuth W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of increasing the size of the valve-guide boss on the exhaust-valve temperature and the volumetric efficiency of an aircraft cylinder

Effect of increasing the size of the valve-guide boss on the exhaust-valve temperature and the volumetric efficiency of an aircraft cylinder

Date: February 1, 1945
Creator: Peters, Max D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Construction of wire strain gages for engine application

Construction of wire strain gages for engine application

Date: December 1, 1943
Creator: Tucker, Maurice
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Continuous use of internal cooling to suppress knock in aircraft engines cruising at high power

Continuous use of internal cooling to suppress knock in aircraft engines cruising at high power

Date: August 1, 1944
Creator: Bell, Arthur H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Determination of gas temperatures from the frequency of knock-induced gas vibrations in an internal-combustion engine

Determination of gas temperatures from the frequency of knock-induced gas vibrations in an internal-combustion engine

Date: January 1, 1946
Creator: Evvard, J C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of carburetor-air temperature on the cooling characteristics of a typical air-cooled engine cylinder

The effect of carburetor-air temperature on the cooling characteristics of a typical air-cooled engine cylinder

Date: September 1, 1945
Creator: Buckner, Howard A , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of carburetor throttle settings on the velocity distribution at the outlet of a vaned and vaneless supercharger inlet elbow

The effect of carburetor throttle settings on the velocity distribution at the outlet of a vaned and vaneless supercharger inlet elbow

Date: September 1, 1945
Creator: Baas, Edmund J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of engine conditions on the lead susceptibility of paraffinic fuels

The effect of engine conditions on the lead susceptibility of paraffinic fuels

Date: October 1, 1944
Creator: Imming, Harry S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of compression ratio, cooled exhaust gas mixed with inlet air, and inlet-air temperature on the knock-limited performance of a full-scale single-cylinder engine

The effect of compression ratio, cooled exhaust gas mixed with inlet air, and inlet-air temperature on the knock-limited performance of a full-scale single-cylinder engine

Date: March 1, 1944
Creator: Breitwieser, Roland
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of continuous knock on the endurance of an aircraft engine cylinder

The effect of continuous knock on the endurance of an aircraft engine cylinder

Date: March 1, 1944
Creator: Peters, M D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of coaxial lapping of cast-iron piston rings on ring performance

Effect of coaxial lapping of cast-iron piston rings on ring performance

Date: April 1, 1944
Creator: Wilson, John G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effects of an increase in the concentration of ethylene dibromide in a leaded fuel on lead deposition, corrosion of exhaust valves, and knock-limited power

The effects of an increase in the concentration of ethylene dibromide in a leaded fuel on lead deposition, corrosion of exhaust valves, and knock-limited power

Date: June 1, 1945
Creator: Zipkin, M A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Correlation of single-cylinder cooling tests of a Pratt and Whitney R-2800-21 engine cylinder with wind-tunnel tests of a Pratt and Whitney R-2800-27 engine

Correlation of single-cylinder cooling tests of a Pratt and Whitney R-2800-21 engine cylinder with wind-tunnel tests of a Pratt and Whitney R-2800-27 engine

Date: December 1, 1943
Creator: Rollin, Vern G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine II

A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine II

Date: June 1, 1946
Creator: Evvard, John C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Cylinder temperatures of two liquid-cooled aircraft cylinders for various engine and coolant conditions

Cylinder temperatures of two liquid-cooled aircraft cylinders for various engine and coolant conditions

Date: October 1, 1945
Creator: Bernardo, Everett
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a full-span retractable flap in combination with full-span plain and internally balanced ailerons on a tapered wing

Wind-tunnel investigation of a full-span retractable flap in combination with full-span plain and internally balanced ailerons on a tapered wing

Date: August 1, 1943
Creator: Fischel, Jack
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables of stiffness and carry-over factor for flat rectangular plates under compression

Tables of stiffness and carry-over factor for flat rectangular plates under compression

Date: November 1, 1943
Creator: Kroll, W D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of effect of sideslip on lateral stability characteristics I : circular fuselage with variations in vertical-tail area and tail length with and without horizontal tail surface

Investigation of effect of sideslip on lateral stability characteristics I : circular fuselage with variations in vertical-tail area and tail length with and without horizontal tail surface

Date: May 1, 1944
Creator: Maclachlan, Robert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of effect of sideslip on lateral stability characteristics III : rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface

Investigation of effect of sideslip on lateral stability characteristics III : rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface

Date: August 1, 1945
Creator: Hollingworth, Thomas A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of effect of sideslip on lateral stability characteristics II : rectangular midwing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface

Investigation of effect of sideslip on lateral stability characteristics II : rectangular midwing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface

Date: April 1, 1945
Creator: Hollingworth, Thomas A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Notes on the propeller and slipstream in relation to stability

Notes on the propeller and slipstream in relation to stability

Date: October 1, 1944
Creator: Ribner, Herbert S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel tests of spoilers on tail surfaces

Wind-tunnel tests of spoilers on tail surfaces

Date: August 1, 1945
Creator: Liddell, Robert B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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