Cover Image

Stability of structural members under axial load.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1937.
Subjects:	Engineering. Aeronautics > Research. Mathematical models.
Online Access:	Electronic resource (PDF)

Similar Items

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

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

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

The stress criterion of a tension member with graded flexural stiffness (contribution to the problem of "clamping effect" outside of the elastic range).
Published: (1936)

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

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

Torsional stability of aluminum alloy seamless tubing.
Published: (1939)

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

The frequency of torsional vibration of a tapered beam.
Published: (1939)

Air flow in a separating laminar boundary layer.
Published: (1935)

A semi℗--graphical method for analyzing strains measured on three or four gage lines intersecting at 45℗ʻ.
Published: (1939)

Charts for checking the stability of compression members in trusses.
Published: (1936)

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

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

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

Heat-stressed structural components in combustion-engine design.
Published: (1938)

Span load distribution for tapered wings with partial℗--span flaps.
Published: (1936)

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

Empirical corrections to the span load distribution at the tip.
Published: (1937)

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

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

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

Theoretical span loading and moments of tapered wings produced by aileron deflection.
Published: (1937)

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

Twisting failure of centrally loaded open-section columns in elastic range.
Published: (1938)

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

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

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

Design of centrifugal impeller blades.
Published: (1939)

Ice formation on wings.
Published: (1939)

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

Two℗--dimensional subsonic compressible flow past elliptic cylinders.
Published: (1938)

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

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

Twisting of thin-walled, stiffened circular cylinders.
Published: (1938)

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

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

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

Combined beam℗--column stresses of aluminum-alloy channel sections.
Published: (1939)

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