Cover Image

Stress concentration around open circular hole in plate subjected to bending normal to plane of plate.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1939.
Subjects:	Aeronautics. Aeronautics > Research. Metals.
Online Access:	Electronic resource (PDF)

Similar Items

Flow phenomena on plates and airfoils of short span.
Published: (1936)

Increase in frictional resistance caused by various types of rivet heads as determined by tests of planing surfaces.
Published: (1938)

Measurement of the air-flow velocity in the cylinder of an airplane engine.
Published: (1939)

Wind℗-tunnel tests of 10-foot-diameter autogiro rotors.
Published: (1936)

Modern methods of fuel testing.
Published: (1939)

A study of unsymmetrical-loading conditions.
Published: (1940)

Stability of castering wheels for aircraft landing gears.
Published: (1940)

Effect of air℗--passage length on optimum fin spacing for maximum cooling.
Published: (1938)

Local instability of symmetrical rectangular tubes under axial compression.
Published: (1939)

Strength of welded aircraft joints.
Published: (1936)

Flight tests of an airplane showing dependence of the maximum lift coefficient on the test conditions.
Published: (1937)

Fatigue testing of wing beams by resonance method.
Published: (1938)

Blower cooling of finned cylinders.
Published: (1936)

Ground-handling forces on a 1/40-scale model of the U. S. airship "Akron".
Published: (1936)

Principles involved in cooling of finned and baffled cylinder.
Published: (1938)

Performance characteristics of Venturi tubes used in aircraft for operating air-driven gyroscopic instruments.
Published: (1937)

Spinning characteristics of wings I--rectangular cark Y monoplane wing.
Published: (1934)

Flight measurements of dynamic longitudinal stability of several airplanes and correlation of measurements with pilots' observations of handling characteristics.
Published: (1936)

Cooling characteristics of 2-row radial engine.
Published: (1935)

Full-scale wind-tunnel and flight tests of a Fairchild 22 airplane equipped with external-airfoil flaps.
Published: (1937)

Pressure distribution over rectangular airfoil with partial-span split flap.
Published: (1936)

Photoelastic analysis of 3-dimensional stress systems using scattered light.
Published: (1939)

Maximum forces applied by pilots to wheel-type controls.
Published: (1937)

Pressure distribution over airfoil section with flap and tab.
Published: (1936)

Bibliography of Aeronautics, 1932.
Published: (1936)

A study of unsymmetrical-loading conditions.
Published: (1940)

Effect of spark-timing regularity on knock limitations of engine performance.
Published: (1938)

Bibliography of Aeronautics, 1931.
Published: (1935)

Chief characteristics and advantages of tailless airplanes.
Published: (1936)

Contribution to the problem of airfoils spanning a free jet.
Published: (1936)

Aerodynamic characteristics of N. A. C. A. 23012 and 23021 airfoils with 20-percent-chord external-airfoil flaps of N. A. C. A. 23012 section.
Published: (1936)

Wind℗--tunnel tests of 3 lateral-control devices in combination with full℗--span slotted flap on N. A. C. A. 23012 airfoil.
Published: (1938)

Experimental investigation of Robinson-type cup anemometer.
Published: (1934)

Generalized analysis of experimental observations in problems of elastic stability.
Published: (1938)

Improved apparatus for measurement of fluctuations of air speed in turbulent flow.
Published: (1932)

Theory for primary failure of straight centrally loaded columns.
Published: (1936)

Lift distribution of wings with end plates.
Published: (1938)

Bending of rectangular plates with large deflections /
by: Levy, Samuel
Published: (1942)

Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression.
Published: (1939)

Limit of stability of curved plate strip under shear and axial stresses.
Published: (1939)