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  Partner: UNT Libraries Government Documents Department
 Year: 1945
 Serial/Series Title: NACA Restricted Bulletin
 Collection: Technical Report Archive and Image Library
An approximate determination of the power required to move control surfaces as related to control-booster design

An approximate determination of the power required to move control surfaces as related to control-booster design

Date: September 1, 1945
Creator: Johnson, Harold I
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
A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane

A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane

Date: August 1, 1945
Creator: Johnson, Harold I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of structural efficiencies of diagonal-tension webs and truss webs of 24S-T aluminum alloy

Comparison of structural efficiencies of diagonal-tension webs and truss webs of 24S-T aluminum alloy

Date: July 1, 1945
Creator: Ochiltree, David W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Computation of the mean tangential velocity of the air leaving the blade tips of a centrifugal supercharger

Computation of the mean tangential velocity of the air leaving the blade tips of a centrifugal supercharger

Date: August 1, 1945
Creator: Brown, W Byron
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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
Dilution of exhaust-gas samples from a multicylinder engine equipped with an exhaust-gas collector

Dilution of exhaust-gas samples from a multicylinder engine equipped with an exhaust-gas collector

Date: February 1, 1945
Creator: Butze, Helmut F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners I : panels with close stiffener spacing that fail by local buckling

Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners I : panels with close stiffener spacing that fail by local buckling

Date: August 1, 1945
Creator: Hickman, William A
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
Fuel-evaporation loss as determined by the change in the specific gravity of the fuel in an aircraft fuel tank

Fuel-evaporation loss as determined by the change in the specific gravity of the fuel in an aircraft fuel tank

Date: May 1, 1945
Creator: Kramer, Walter E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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