You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Year: 1946
 Serial/Series Title: NACA Restricted Bulletin
 Collection: National Advisory Committee for Aeronautics Collection
Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades

Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades

Date: February 1, 1946
Creator: Rice, Fred J , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the fatigue life of an airplane wing structure under overload conditions

An analysis of the fatigue life of an airplane wing structure under overload conditions

Date: February 1, 1946
Creator: Reisert, Thomas D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of fuel-vapor loss on knock-limited performance and inspection properties of aviation fuels

Effects of fuel-vapor loss on knock-limited performance and inspection properties of aviation fuels

Date: March 1, 1946
Creator: Marsh, Edred T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Knock-Limited Performance of Fuel Blends Containing Spiropentane, Methylenecyclobutane, Di-Tert-Butyl Ether, Methyl Tert-Butyl Ether, and Triptane

The Knock-Limited Performance of Fuel Blends Containing Spiropentane, Methylenecyclobutane, Di-Tert-Butyl Ether, Methyl Tert-Butyl Ether, and Triptane

Date: May 1, 1946
Creator: Meyer, Carl L.
Description: Tests show that at inlet-air temperatures of 250 deg F and 100 deg F the knock-limited performance of the base fuel of blends, leaded with 4 ml TEL per gallon and containing 20 percent spiropentane, was reduced at fuel/air ratios below 0.085. The 20 percent methylenecyclobutane reduced the knock-limited power of the base fuel at fuel/air ratios below 0.112. Di-tert-butyl ether, methyl-tert-butyl ether, and triptane increased the knock-limited power of the base fuel at all fuel/air ratios and at both temperatures.
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
Static-pressure error of an airspeed installation on an airplane in high-speed dives and pullouts

Static-pressure error of an airspeed installation on an airplane in high-speed dives and pullouts

Date: February 1, 1946
Creator: Wood, Clotaire
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 6 degrees and 9 degrees trim and a 22-1/2 degree angle of dead rise

Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 6 degrees and 9 degrees trim and a 22-1/2 degree angle of dead rise

Date: February 1, 1946
Creator: Stewart, Thelma
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 12 degree trim and with a 22-1/2 degree angle of dead rise

Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 12 degree trim and with a 22-1/2 degree angle of dead rise

Date: February 1, 1946
Creator: Batterson, Sidney A
Description: None
Contributing Partner: UNT Libraries Government Documents Department