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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Restricted Bulletin
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
Computation of the mean tangential velocity of the air leaving the blade tips of a centrifugal supercharger

Computation of the mean tangential velocity of the air leaving the blade tips of a centrifugal supercharger

Date: August 1, 1945
Creator: Brown, W Byron
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
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
Dilution of exhaust-gas samples from a multicylinder engine equipped with an exhaust-gas collector

Dilution of exhaust-gas samples from a multicylinder engine equipped with an exhaust-gas collector

Date: February 1, 1945
Creator: Butze, Helmut F
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
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
Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds

Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds

Date: July 1, 1945
Creator: Katzoff, S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Notes on the skipping of seaplanes

Notes on the skipping of seaplanes

Date: September 1, 1943
Creator: Parkinson, John B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 3 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 3 degree trim and with a 22 1/2 degree angle of dead rise

Date: February 1, 1945
Creator: Batterson, Sidney A
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
XC-35 gust research project analysis of gust measurements

XC-35 gust research project analysis of gust measurements

Date: April 1, 1944
Creator: Moskovitz, A I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
XC-35 gust research project characteristics of vertical drafts and associated vertical gust velocities within convective type clouds

XC-35 gust research project characteristics of vertical drafts and associated vertical gust velocities within convective type clouds

Date: February 1, 1945
Creator: Moskovitz, A I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of structural efficiencies of diagonal-tension webs and truss webs of 24S-T aluminum alloy

Comparison of structural efficiencies of diagonal-tension webs and truss webs of 24S-T aluminum alloy

Date: July 1, 1945
Creator: Ochiltree, David W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane

A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane

Date: August 1, 1945
Creator: Johnson, Harold I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Notes on unusual V-G records from transport airplanes

Notes on unusual V-G records from transport airplanes

Date: August 1, 1944
Creator: Walker, Walter G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An approximate method of shear-lag analysis for beams loaded at right angles to the plane of symmetry of the cross section

An approximate method of shear-lag analysis for beams loaded at right angles to the plane of symmetry of the cross section

Date: September 1, 1943
Creator: Brilmyer, Harold J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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
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
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
Shear tests on DuPont explosive rivets with the countersunk head milled flush after expansion

Shear tests on DuPont explosive rivets with the countersunk head milled flush after expansion

Date: May 1, 1943
Creator: Bartone, Leonard M
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
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