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Partner:
UNT Libraries Government Documents Department
Year:
1946
Language:
English
Serial/Series Title:
NACA Restricted Bulletin
Serial/Series Title:
NACA Wartime Reports
Collection:
National Advisory Committee for Aeronautics Collection
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61378/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61278/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc62314/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc62316/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc62308/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc62411/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61794/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61797/