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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
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
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
Early detection of cracks resulting from fatigue stressing

Early detection of cracks resulting from fatigue stressing

Date: September 1, 1944
Creator: Bennett, John A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of beams having webs with large circular lightening holes

Tests of beams having webs with large circular lightening holes

Date: February 1, 1944
Creator: Levin, L Ross
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
Determination of iron contamination of used lubricating oil for use in measuring rates of wear in aircraft engines

Determination of iron contamination of used lubricating oil for use in measuring rates of wear in aircraft engines

Date: March 1, 1944
Creator: Tischler, Adelbert O
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
End-zone water injection as a means of suppressing knock in a spark-ignition engine

End-zone water injection as a means of suppressing knock in a spark-ignition engine

Date: September 1, 1944
Creator: Miller, Cearcy D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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