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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Wartime Reports
 Collection: Technical Report Archive and Image Library
A metallurgical investigation of a large forged disc of CSA (234-A-5) alloy

A metallurgical investigation of a large forged disc of CSA (234-A-5) alloy

Date: October 1, 1945
Creator: White, A E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The rupture test characteristics of six precision- cast and three wrought alloys at 1700 and 1800 F

The rupture test characteristics of six precision- cast and three wrought alloys at 1700 and 1800 F

Date: November 1, 1945
Creator: White, A E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight and test-stand investigation of high-performance fuels in modified double-row radial air-cooled engines I : determination of the cooling characteristics of the flight engine

Flight and test-stand investigation of high-performance fuels in modified double-row radial air-cooled engines I : determination of the cooling characteristics of the flight engine

Date: July 1, 1945
Creator: White, H Jack
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of water injection to decrease gasoline consumption in an aircraft engine cruising at high power

Use of water injection to decrease gasoline consumption in an aircraft engine cruising at high power

Date: August 1, 1944
Creator: White, H Jack
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Correlation of mixture temperature data obtained from bare intake-manifold thermocouples

Correlation of mixture temperature data obtained from bare intake-manifold thermocouples

Date: January 1, 1946
Creator: White, H. Jack & Gammon, Goldie L
Description: A relatively simple equation has been found to express with fair accuracy, variation in manifold-charge temperature with charge in engine operating conditions. This equation and associated curves have been checked by multi cylinder-engine data, both test stand and flight, over a wide range of operating conditions. Average mixture temperatures, predicted by the equations of this report, agree reasonably well with results within the same range of carburetor-air temperatures from laboratories and test stands other than the NACA.
Contributing Partner: UNT Libraries Government Documents Department
Flight Investigation of Wing-Gun Fairings on a Fighter Type Airplane

Flight Investigation of Wing-Gun Fairings on a Fighter Type Airplane

Date: October 1, 1941
Creator: White, M D
Description: Description is given of flight tests conducted on gun fairings, designed to correct the detrimental effects of the projecting and submerged wing guns on an F4F-3 fighter. It was found that the installation of unfaired guns on a clean wing resulted in a premature stall that increased the stalling speed in the carrier-approach and landing conditions of flight by suitably fairing the guns, it was possible to reduce the stalling speeds to values approaching very nearly the clean-wing values.
Contributing Partner: UNT Libraries Government Documents Department
Effect of power on the stick-fixed neutral points of several single-engine monoplanes as determined in flight

Effect of power on the stick-fixed neutral points of several single-engine monoplanes as determined in flight

Date: August 1, 1944
Creator: White, Maurice D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Estimation of stick-fixed neutral points of airplanes

Estimation of stick-fixed neutral points of airplanes

Date: March 1, 1945
Creator: White, Maurice D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight tests of NACA jet-propulsion exhaust stacks on the supermarine spitfire airplane

Flight tests of NACA jet-propulsion exhaust stacks on the supermarine spitfire airplane

Date: December 1, 1942
Creator: White, Maurice D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Lateral-control characteristics of North American XP-51 airplane (A. C. No. 41-38) with beveled trailing-edge ailerons in high-speed flight

Lateral-control characteristics of North American XP-51 airplane (A. C. No. 41-38) with beveled trailing-edge ailerons in high-speed flight

Date: November 1, 1942
Creator: White, Maurice D
Description: None
Contributing Partner: UNT Libraries Government Documents Department