Calculation of load distribution in stiffened cylindrical shells.
| Corporate Author: | United States. National Advisory Committee for Aeronautics |
|---|---|
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington] :
[s.n.],
1938.
|
| Subjects: | |
| Online Access: | Electronic resource (PDF) |
Similar Items
Load tests on stiffened circular cylindrical shell.
Published: (1938)
Published: (1938)
Loads imposed on intermediate frames of stiffened shells.
Published: (1939)
Published: (1939)
Methods and formulas for calculating the strength of plate and shell constructions as used in airplane design.
Published: (1936)
Published: (1936)
A method of estimating the critical buckling load for structural members.
Published: (1939)
Published: (1939)
Span load distribution for tapered wings with partial℗--span flaps.
Published: (1936)
Published: (1936)
Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression.
Published: (1939)
Published: (1939)
Calculation of chord-wise load distribution over air℗-foil sections with plain, split, or serially hinged trailing℗--edge flaps.
Published: (1938)
Published: (1938)
Stresses in reinforcing rings due to axial forces in cylindrical and conical stressed skins.
Published: (1938)
Published: (1938)
A simplified method for the calculation of airfoil pressure distribution.
Published: (1939)
Published: (1939)
Calculation of induced efficiency of heavily loaded propellers having infinite number of blades; Induced efficiency of optimum propellers having finite number of blades; Prospects of propeller drive for high flying speeds.
Published: (1939)
Published: (1939)
Theoretical study of various airplane motions after initial disturbance.
Published: (1938)
Published: (1938)
Compression struts with nonprogressively variable moment of inertia.
Published: (1938)
Published: (1938)
Study of torque equilibrium of autogiro rotor.
Published: (1938)
Published: (1938)
Behavior of plate strip under shear and compressive stresses beyond buckling limit.
Published: (1938)
Published: (1938)
On the determination of the take℗--off characteristics of a seaplane.
Published: (1938)
Published: (1938)
Behavior of static pressure heads at high speeds.
Published: (1938)
Published: (1938)
Operational treatment of nonuniform-lift theory in airplane dynamics.
Published: (1938)
Published: (1938)
Design of centrifugal impeller blades.
Published: (1939)
Published: (1939)
Ice formation on wings.
Published: (1939)
Published: (1939)
Potential flow about arbitrary biplane wing sections.
Published: (1935)
Published: (1935)
Torsional stability of aluminum alloy seamless tubing.
Published: (1939)
Published: (1939)
Considerations affecting the additional weight required in mass balance of ailerons.
Published: (1937)
Published: (1937)
Theory of two-dimensional potential flow about arbitrary wing sections.
Published: (1939)
Published: (1939)
Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law.
Published: (1937)
Published: (1937)
An analysis of longitudinal stability in power-off flight with charts for use in design.
Published: (1935)
Published: (1935)
Comparison of theory with experiment in phenomenom of wing flutter.
Published: (1939)
Published: (1939)
The impact on floats or hulls during landing as affected by bottom width.
Published: (1936)
Published: (1936)
Analysis of 3 lowest bending frequencies of rotating propeller.
Published: (1936)
Published: (1936)
Theory of automatic control of airplanes.
Published: (1939)
Published: (1939)
Investigations on the amount of downwash behind rectangular and elliptical wings.
Published: (1936)
Published: (1936)
Experimental studies of the effective width of buckled sheets.
Published: (1936)
Published: (1936)
General considerations on the flow of compressible fluids.
Published: (1936)
Published: (1936)
The strength of shell bodies--theory and practice.
Published: (1937)
Published: (1937)
A simplified application of the method of operators to the calculation of disturbed motions of an airplane.
Published: (1936)
Published: (1936)
Theoretical span loading and moments of tapered wings produced by aileron deflection.
Published: (1937)
Published: (1937)
Pressure distribution over airfoils with Fowler flaps.
Published: (1937)
Published: (1937)
On the actual loads on airplane landing gears.
Published: (1937)
Published: (1937)
Analysis of 2-spar cantilever wings with special reference to torsion and load transference.
Published: (1934)
Published: (1934)
Investigation of lift distribution over the separate wings of biplane.
Published: (1939)
Published: (1939)
The variation with Reynolds number of pressure distribution over an airfoil section.
Published: (1938)
Published: (1938)