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  Partner: UNT Libraries Government Documents Department
 Year: 1944
 Serial/Series Title: NACA Restricted Bulletin
 Collection: Technical Report Archive and Image Library
Maximum lift coefficients of airplanes based on sum of wing and tail areas

Maximum lift coefficients of airplanes based on sum of wing and tail areas

Date: March 1, 1944
Creator: Ankenbruck, Herman O
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary investigation of the relation of the compressive strength of sheet-stiffener panels to the diameter of rivet used for attaching stiffeners to sheet

Preliminary investigation of the relation of the compressive strength of sheet-stiffener panels to the diameter of rivet used for attaching stiffeners to sheet

Date: November 1, 1944
Creator: Hickman, William A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some strength tests of stiffened curved sheets loaded in shear

Some strength tests of stiffened curved sheets loaded in shear

Date: April 1, 1944
Creator: Chiarito, Patrick T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The landing stability of a powered dynamic model of a flying boat with a 30 degree v-step and with two depths of transverse step

The landing stability of a powered dynamic model of a flying boat with a 30 degree v-step and with two depths of transverse step

Date: February 1, 1944
Creator: Land, Norman S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of lateral shift of center of gravity on rudder deflection required for trim

Effect of lateral shift of center of gravity on rudder deflection required for trim

Date: November 1, 1944
Creator: Hunter, P A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A positive-replica technique for examining finished metal surfaces and its application to aircraft engine cylinders

A positive-replica technique for examining finished metal surfaces and its application to aircraft engine cylinders

Date: September 1, 1944
Creator: Clark, Thomas P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Maximum rates of control motion obtained from ground tests

Maximum rates of control motion obtained from ground tests

Date: May 1, 1944
Creator: Beeler, De E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of propeller operation on the distribution of the load on the vertical tail surface of a typical pursuit airplane

Some effects of propeller operation on the distribution of the load on the vertical tail surface of a typical pursuit airplane

Date: March 1, 1944
Creator: Dingeldein, Richard C
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
Effect of inlet-air temperature and cylinder displacement on charge temperature of internal combustion engines

Effect of inlet-air temperature and cylinder displacement on charge temperature of internal combustion engines

Date: January 1, 1944
Creator: Bolz, Ray E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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