Cover Image

Torsional stability of aluminum alloy seamless tubing.

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

Similar Items

Stability of thin℗-walled tubes under torsion.
Published: (1933)

Torsion tests of tubes.
Published: (1937)

An analysis of longitudinal stability in power-off flight with charts for use in design.
Published: (1935)

Frequencies of cantilever wings in beam and torsional vibrations.
Published: (1940)

Torsional and bending deflection of full-scale aluminum℗--alloy propeller blades under normal operating conditions.
Published: (1938)

Analysis of 2-spar cantilever wings with special reference to torsion and load transference.
Published: (1934)

Preliminary fatigue studies on aluminum alloy aircraft girders.
Published: (1938)

Weathering of aluminum alloy sheet materials used in aircraft.
Published: (1934)

The Column Strength of Two Extruded Aluminum-Alloy H-Sections.
Published: (1938)

Column strength of tubes elastically restrained against rotation at the ends.
Published: (1937)

Mechanical properties of aluminum-alloy rivets.
Published: (1936)

Longitudinal stability in relation to use of automatic pilot.
Published: (1938)

Design of centrifugal impeller blades.
Published: (1939)

Ice formation on wings.
Published: (1939)

Theory of two-dimensional potential flow about arbitrary wing sections.
Published: (1939)

Comparison of theory with experiment in phenomenom of wing flutter.
Published: (1939)

A method of estimating the critical buckling load for structural members.
Published: (1939)

Theory of automatic control of airplanes.
Published: (1939)

Theoretical study of various airplane motions after initial disturbance.
Published: (1938)

Potential flow about arbitrary biplane wing sections.
Published: (1935)

Considerations affecting the additional weight required in mass balance of ailerons.
Published: (1937)

Compression struts with nonprogressively variable moment of inertia.
Published: (1938)

Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law.
Published: (1937)

Methods and formulas for calculating the strength of plate and shell constructions as used in airplane design.
Published: (1936)

Calculation of load distribution in stiffened cylindrical shells.
Published: (1938)

Study of torque equilibrium of autogiro rotor.
Published: (1938)

Behavior of plate strip under shear and compressive stresses beyond buckling limit.
Published: (1938)

The impact on floats or hulls during landing as affected by bottom width.
Published: (1936)

Analysis of 3 lowest bending frequencies of rotating propeller.
Published: (1936)

On the determination of the take℗--off characteristics of a seaplane.
Published: (1938)

Behavior of static pressure heads at high speeds.
Published: (1938)

Operational treatment of nonuniform-lift theory in airplane dynamics.
Published: (1938)

Investigations on the amount of downwash behind rectangular and elliptical wings.
Published: (1936)

Experimental studies of the effective width of buckled sheets.
Published: (1936)

General considerations on the flow of compressible fluids.
Published: (1936)

Static longitudinal stability and longitudinal control of autogiro rotors.
Published: (1938)

Crinkling strength and bending strength of round aircraft tubing.
Published: (1938)

Increasing the strength of aluminum-alloy columns by prestressing.
Published: (1937)

Analysis of lateral stability in power-off flight with charts for use in design.
Published: (1936)

Effect of compressibility on pressure reading of Prandtl pitot tube at subsonic flow velocity.
Published: (1939)