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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Restricted Bulletin
 Collection: Technical Report Archive and Image Library
Determination from flight tests of thrust coefficients for 10 full-scale airplanes in the gliding condition with engine idling

Determination from flight tests of thrust coefficients for 10 full-scale airplanes in the gliding condition with engine idling

Date: June 1, 1945
Creator: Talmage, Donald B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube

Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube

Date: April 1, 1945
Creator: Humphreys, Milton D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparative fatigue tests of riveted joints of Alclad 24S-T, Alclad 24S-T81, Alclad 24S-RT, Alclad 24S-T86 and Alclad 75S-T sheet

Comparative fatigue tests of riveted joints of Alclad 24S-T, Alclad 24S-T81, Alclad 24S-RT, Alclad 24S-T86 and Alclad 75S-T sheet

Date: August 1, 1945
Creator: Mill, M N
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An electronic indicator for angular velocity and acceleration

An electronic indicator for angular velocity and acceleration

Date: August 1, 1944
Creator: Krebs, Richard P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of oil consumption and piston cooling on knock-limited aircraft-engine performance

The effect of oil consumption and piston cooling on knock-limited aircraft-engine performance

Date: May 1, 1944
Creator: Richard, Paul H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Pressure lag in tubing used in flight research

Pressure lag in tubing used in flight research

Date: January 1, 1945
Creator: Turner, Howard L & Rathert, George A , Jr
Description: Tests described in this report were undertaken to obtain a quantitative measure of the pressure lag in typical pressure-tubing systems used by the Ames Aeronautical Laboratory in flight research investigations. Lag measurements were made with both single-direction and oscillating pressure changes. Single-direction pressure changes were investigated to determine if the lag in orifice-pressure lines and in the research airspeed and altitude measuring systems of pursuit-type airplane undergoing flight tests was sufficient to cause an appreciable error in the record of a sudden pressure change. Oscillating pressure changes were investigated with particular reference to the accuracy of pressure peaks in pressure-distribution measurements during the time of buffeting conditions as found in stalls. (author).
Contributing Partner: UNT Libraries Government Documents Department
A method for the determination of aromatics in hydrocarbon mixtures

A method for the determination of aromatics in hydrocarbon mixtures

Date: December 1, 1945
Creator: Hipsher, Harold F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Lead susceptibility of several fuels as determined in an air-cooled aircraft-engine cylinder

Lead susceptibility of several fuels as determined in an air-cooled aircraft-engine cylinder

Date: February 1, 1946
Creator: Hensley, Reece V
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of the characteristics of a propeller alcohol feed ring

An investigation of the characteristics of a propeller alcohol feed ring

Date: June 1, 1944
Creator: Neel, Carr B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Thermodynamic design of double-panel, air-heated windshields for ice prevention

Thermodynamic design of double-panel, air-heated windshields for ice prevention

Date: June 1, 1943
Creator: Kushnick, Jerome L
Description: None
Contributing Partner: UNT Libraries Government Documents Department