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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
An automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane

An automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane

Date: May 1, 1944
Creator: Gillis, Clarence L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculation of stick forces for an elevator with a spring tab

Calculation of stick forces for an elevator with a spring tab

Date: June 1, 1944
Creator: Greenberg, Harry
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculations of intake-air cooling resulting from water injection and of water recovery from exhaust gas

Calculations of intake-air cooling resulting from water injection and of water recovery from exhaust gas

Date: August 1, 1944
Creator: Rotherock, Addison M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparative tests of the strength and tightness of commercial flush rivets of one type and NACA flush rivets in machine-countersunk and counterpunched joints

Comparative tests of the strength and tightness of commercial flush rivets of one type and NACA flush rivets in machine-countersunk and counterpunched joints

Date: February 1, 1944
Creator: Mandel, Merven W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Cylinder-head cooling by means of a shield in the exhaust passage

Cylinder-head cooling by means of a shield in the exhaust passage

Date: June 1, 1944
Creator: Mulcahy, B A & Wilsted, H D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Determination of desirable lengths of Z- and channel-section columns for local-instability tests

Determination of desirable lengths of Z- and channel-section columns for local-instability tests

Date: October 1, 1944
Creator: Roy, J Albert
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
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
The effect of angle of bend between plate elements on the local instability of formed Z-sections

The effect of angle of bend between plate elements on the local instability of formed Z-sections

Date: September 1, 1944
Creator: Schuette, Evan H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of Changes in Aileron Rigging on the Stick Forces of a High-Speed Fighter Airplane

Effect of Changes in Aileron Rigging on the Stick Forces of a High-Speed Fighter Airplane

Date: May 1, 1944
Creator: Murray, Harry E. & Warren, S Anne
Description: The effects of changes in aileron rigging between 2 deg up and 2 deg down on the stick forces were determined from wind-tunnel data for a finite-span wing model. These effects were investigated for ailerons deflecting equally in both directions and linearly with stick deflection. Data were analyzed for a Frise, a sealed internally balanced, and a beveled-trailing-edge aileron. The results of the analysis showed that only ailerons having linear hinge-moment characteristics are unaffected by changes in rigging and indicated that ailerons having decidedly nonlinear hinge-moment-coefficient curves, particularly for deflections near 0 deg, are very sensitive to changes in rigging.
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
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
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
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
An estimation of the internal-cooling requirements of an aircraft-engine cylinder when using oxygen boost

An estimation of the internal-cooling requirements of an aircraft-engine cylinder when using oxygen boost

Date: November 1, 1944
Creator: Moeckel, W E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight investigation at high Mach numbers of several methods of measuring static pressure on an airplane wing

Flight investigation at high Mach numbers of several methods of measuring static pressure on an airplane wing

Date: November 1, 1944
Creator: Daum, Fred L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat-capacity lag in turbine-working fluids

Heat-capacity lag in turbine-working fluids

Date: May 1, 1944
Creator: Huber, Paul W
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
The knock-limited performance of several fuels blended with S-2 reference fuel

The knock-limited performance of several fuels blended with S-2 reference fuel

Date: November 1, 1944
Creator: Alquist, Henry E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Landing characteristics of a model of a flying boat with the depth of step reduced to zero by means of a retractable planing flap

Landing characteristics of a model of a flying boat with the depth of step reduced to zero by means of a retractable planing flap

Date: February 1, 1944
Creator: Freihofner, Anton
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
Material properties of two types of plastic-bonded glass cloth

Material properties of two types of plastic-bonded glass cloth

Date: December 1, 1944
Creator: Schuette, Evan H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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
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