Cover Image

Method of curved models and its application to the study of curvilinear flight of airships, pt. 1.

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

Similar Items

Method of curved models and its application to the study of curvilinear flight of airships, pt. 2.
Published: (1937)

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

The question of spontaneous wing oscillations (determination of critical velocity through flight-oscillation tests).
Published: (1936)

Improvement of aileron effectiveness by prevention of air leakage through hinge gap as determined in flight.
Published: (1938)

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

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

Procedure for determining speed and climbing performance of airships.
Published: (1936)

The gyroplane--its principles and its possibilities.
Published: (1937)

Adhesion of ice in its relation to de℗--icing of airplanes.
Published: (1939)

Behavior of turbulent boundary layers on curved convex walls.
Published: (1936)

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

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

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

The ground effect on lifting propellers.
Published: (1937)

Aerodynamic characteristics of full℗--scale propellers having 2, 3, and 4 blades of Clark Y and R. A. F. 6 airfoil sections.
Published: (1937)

The scale effect in towing tests with airplane-float systems.
Published: (1937)

Study of factors affecting range of airplanes.
Published: (1937)

Pressure distribution over Clark Y-H airfoil section with split flap.
Published: (1937)

Turbulent boundary layer of an airfoil.
Published: (1937)

On the actual loads on airplane landing gears.
Published: (1937)

Experimental and calculated characteristics of 22 tapered wings [aircraft].
Published: (1937)

Charts for checking the stability of plane systems of rods.
Published: (1937)

Torsion tests of tubes.
Published: (1937)

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

Contributions to the theory of incomplete tension bay.
Published: (1937)

The strength of shell bodies--theory and practice.
Published: (1937)

Transition phase in take-off of airplane.
Published: (1937)

A simplified method for the calculation of airfoil pressure distribution.
Published: (1939)

N.A.C.A. Stall-warning indicator.
Published: (1938)

Airfoil section characteristics as applied to prediction of air forces and their distribution on wings.
Published: (1938)

Effect of compressibility on 8 full-scale propellers operating in take℗--off and climbing range.
Published: (1938)

Pressure℗--distribution investigation of an N. A. C. A. 0009 airfoil with 50-percent-chord plain flap and three tabs.
Published: (1939)

Calculation of chord-wise load distribution over air℗-foil sections with plain, split, or serially hinged trailing℗--edge flaps.
Published: (1938)

An approximate spin design criterion for monoplanes.
Published: (1939)

Tests of N. A. C. A. 23012 airfoil with slotted deflector flap.
Published: (1939)

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

Wind-tunnel investigation of ground effect on wings with flaps.
Published: (1939)

Tank tests of model 36 flying-boat hull.
Published: (1938)

Wind℗--tunnel investigation of effect of yaw on lateral-stability characteristics : 1, Four N. A. C. A. 23012 wings of various plan forms with and without dihedral.
Published: (1939)

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