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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Restricted Bulletin
 Collection: Technical Report Archive and Image Library
Calculations of intake-air cooling resulting from water injection and of water recovery from exhaust gas
No Description digital.library.unt.edu/ark:/67531/metadc61929/
Computation of the mean tangential velocity of the air leaving the blade tips of a centrifugal supercharger
No Description digital.library.unt.edu/ark:/67531/metadc62510/
Effect of inlet-air temperature and cylinder displacement on charge temperature of internal combustion engines
No Description digital.library.unt.edu/ark:/67531/metadc61864/
Determination of iron contamination of used lubricating oil for use in measuring rates of wear in aircraft engines
No Description digital.library.unt.edu/ark:/67531/metadc62322/
Dilution of exhaust-gas samples from a multicylinder engine equipped with an exhaust-gas collector
No Description digital.library.unt.edu/ark:/67531/metadc62393/
Effects of fuel-vapor loss on knock-limited performance and inspection properties of aviation fuels
No Description digital.library.unt.edu/ark:/67531/metadc62314/
Cylinder-head cooling by means of a shield in the exhaust passage
No Description digital.library.unt.edu/ark:/67531/metadc61930/
Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds
No Description digital.library.unt.edu/ark:/67531/metadc61260/
Notes on the skipping of seaplanes
No Description digital.library.unt.edu/ark:/67531/metadc60899/
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
No Description digital.library.unt.edu/ark:/67531/metadc61796/
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
No Description 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
No Description digital.library.unt.edu/ark:/67531/metadc61797/
XC-35 gust research project analysis of gust measurements
No Description digital.library.unt.edu/ark:/67531/metadc61106/
XC-35 gust research project characteristics of vertical drafts and associated vertical gust velocities within convective type clouds
No Description digital.library.unt.edu/ark:/67531/metadc61108/
Comparison of structural efficiencies of diagonal-tension webs and truss webs of 24S-T aluminum alloy
No Description digital.library.unt.edu/ark:/67531/metadc60972/
A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane
No Description digital.library.unt.edu/ark:/67531/metadc61000/
Notes on unusual V-G records from transport airplanes
No Description digital.library.unt.edu/ark:/67531/metadc61139/
An approximate method of shear-lag analysis for beams loaded at right angles to the plane of symmetry of the cross section
No Description digital.library.unt.edu/ark:/67531/metadc61305/
An automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane
No Description digital.library.unt.edu/ark:/67531/metadc61488/
Comparative tests of the strength and tightness of commercial flush rivets of one type and NACA flush rivets in machine-countersunk and counterpunched joints
No Description digital.library.unt.edu/ark:/67531/metadc61746/
Landing characteristics of a model of a flying boat with the depth of step reduced to zero by means of a retractable planing flap
No Description digital.library.unt.edu/ark:/67531/metadc61760/
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
No Description digital.library.unt.edu/ark:/67531/metadc60902/
Shear tests on DuPont explosive rivets with the countersunk head milled flush after expansion
No Description digital.library.unt.edu/ark:/67531/metadc61753/
Some effects of propeller operation on the distribution of the load on the vertical tail surface of a typical pursuit airplane
No Description digital.library.unt.edu/ark:/67531/metadc61504/
Use of stagnation temperature in calculating rate of heat transfer in aircraft heat exchangers
No Description digital.library.unt.edu/ark:/67531/metadc62447/
Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight
No Description digital.library.unt.edu/ark:/67531/metadc61599/
The use of geared spring tabs for elevator control
No Description digital.library.unt.edu/ark:/67531/metadc279612/
Tests of beams having webs with large circular lightening holes
No Description digital.library.unt.edu/ark:/67531/metadc62210/
Tests of hydraulically expanded rivets
No Description digital.library.unt.edu/ark:/67531/metadc61749/
Flight investigation at high Mach numbers of several methods of measuring static pressure on an airplane wing
No Description digital.library.unt.edu/ark:/67531/metadc61475/
Spinning of large airplanes
No Description digital.library.unt.edu/ark:/67531/metadc62551/
Tests of 10-inch 24S-T aluminum-alloy shear panels with 1-1/2-inch holes I
No Description digital.library.unt.edu/ark:/67531/metadc62245/
Tests of 10 inch 24S-T aluminum-alloy shear panels with 1-1/2 inch holes II : panels having holes with notched edges
No Description digital.library.unt.edu/ark:/67531/metadc62248/
Flight tests of a glider model towed by twin parallel towlines
No Description digital.library.unt.edu/ark:/67531/metadc62655/
Material properties of two types of plastic-bonded glass cloth
No Description digital.library.unt.edu/ark:/67531/metadc62383/
Test data on the shear strength of joints assembled with round-head and brazier-head rivets
No Description digital.library.unt.edu/ark:/67531/metadc61850/
Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model
No Description digital.library.unt.edu/ark:/67531/metadc61652/
Critical compressive stress for curved sheet supported along all edges and elastically restrained against rotation along the unloaded edges
No Description digital.library.unt.edu/ark:/67531/metadc60915/
Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22-1/2 degrees
No Description digital.library.unt.edu/ark:/67531/metadc61709/
The Effect of Artificial Aging on the Tensile Properties of Alclad 24S-T and 24S-T Aluminum Alloy
An experimental study was made to determine the effect of artificial aging on the tensile properties of alclad 24S-T and 24S-T aluminum-alloy sheet material. The results of the tests show that certain combinations of aging time and temperature cause a marked increase in the yield strength and a small increase in the ultimate strength; these increases are accompanied by a very large decrease in elongation. A curve is presented that shows the maximum yield strengths that can be obtained by aging this material at various combinations of time and temperature. The higher values of yield stress are obtained in material aged at relatively longer times and lower temperatures. digital.library.unt.edu/ark:/67531/metadc62249/
The effect of angle of bend between plate elements on the local instability of formed Z-sections
No Description digital.library.unt.edu/ark:/67531/metadc62250/
An approximate determination of the power required to move control surfaces as related to control-booster design
No Description digital.library.unt.edu/ark:/67531/metadc61654/
Effect of lateral shift of center of gravity on rudder deflection required for trim
No Description digital.library.unt.edu/ark:/67531/metadc61143/
NACA procedure for flight tests of aileron characteristics of airplanes
No Description digital.library.unt.edu/ark:/67531/metadc61631/
Investigation of methods of supporting single-thickness specimens in a fixture for determination of compressive stress-strain curves
No Description digital.library.unt.edu/ark:/67531/metadc62425/
The longitudinal shear strength required in double-angle columns of 24S-T aluminum alloy
No Description digital.library.unt.edu/ark:/67531/metadc62242/
Proposal for a propeller side-force factor
No Description digital.library.unt.edu/ark:/67531/metadc62133/
Resume of hinge-moment data for unshielded horn- balanced control surfaces
No Description digital.library.unt.edu/ark:/67531/metadc61491/
A preliminary study of machine-countersunk flush rivets subjected to a combined static and alternating shear load
No Description digital.library.unt.edu/ark:/67531/metadc61745/
Preliminary tank experiments with a hydrofoil on a planing-tail seaplane hull
No Description digital.library.unt.edu/ark:/67531/metadc61786/
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