Cover Image

Comparison of theory with experiment in phenomenom of wing flutter.

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

Similar Items

Status of wing flutter.
Published: (1936)

Ice formation on wings.
Published: (1939)

General theory of aerodynamic instability and mechanism of flutter.
Published: (1934)

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

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

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

Flight comparison of conventional ailerons on rectangular wing and of conventional and floating wing℗--tip ailerons on tapered wing.
Published: (1937)

Model experiments on forces and moments acting on end plate fitted to wing.
Published: (1938)

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

Performance of rotating-wing aircraft.
Published: (1938)

Wing-nacelle℗--propeller interference for wings of various spans, force, and pressure℗--distribution tests.
Published: (1936)

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

Spinning characteristics of wings : 5, N. A. C. A. 0009, 23018, and 6718 monoplane wings.
Published: (1938)

Effect of slipstream on airplane wing.
Published: (1939)

Spinning characteristics of wings IV : Changes in stagger of rectangular Clark Y biplane cellules.
Published: (1937)

The influence of wing setting on wing load and rotor speed of PCA-2 autogiro as determined in flight.
Published: (1934)

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

Investigation of lift distribution over the separate wings of biplane.
Published: (1939)

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

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

Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails : 1. Basic loading condition.
Published: (1937)

Design of centrifugal impeller blades.
Published: (1939)

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

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

Experiments on a slotted wing.
Published: (1939)

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

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)

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

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)

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

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