Cover Image

Contribution to aerodynamics of rotating-wing aircraft.

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

Similar Items

Contribution to the Aerodynamics of Rotating Wing Aircraft.
Published: (1941)

Aerodynamics of Rotating-Wing Aircraft with Blade-Pitch Control.
Published: (1940)

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

Contribution to the Aerodynamics of Rotating Wing Aircraft.
Published: (1941)

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

Power of aircraft engines at altitude.
Published: (1939)

Aerodynamic characteristics of wings with cambered external-airfoil flaps, including lateral control with full-span flap.
Published: (1935)

The horsepower of aircraft engines and their maximum frontal area.
Published: (1936)

The effects of partial℗--span slotted flaps on aerodynamic characteristics of a rectangular and a tapered N. A. C. A. 23012 wing.
Published: (1939)

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

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)

Interference of wing and fuselage from tests of 8 combinations in N. A. C. A. variable-density tunnel combinations with tapered fillets and straight℗--side juncture.
Published: (1938)

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)

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)

The Oscillating Wing with Aerodynamically Balanced Elevator.
Published: (1941)

Aerodynamic effects of wing cut℗-outs.
Published: (1934)

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

Effects of some common surface irregularities on wing drag.
Published: (1939)

The effects of surface waviness and of rib stitching on wing drag.
Published: (1939)

Experimental and analytical investigation of monocoque wing model loaded in bending.
Published: (1939)

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

The unsteady lift of a finite wing.
Published: (1939)

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

Theoretical stability and control characteristics of wings with various amounts of taper and twist.
Published: (1938)

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

Stability of castering wheels for aircraft landing gears.
Published: (1940)

Aerodynamic characteristics of 4 full℗-scale propellers having different plan forms.
Published: (1937)

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

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

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

Way to increased airplane engine power.
Published: (1939)

Design of N.A.C.A. cowlings for radial air℗--cooled engines.
Published: (1938)

Interrelation of exhaust-gas constituents.
Published: (1937)

Engines and propellers for powered gliders and light airplanes.
Published: (1938)

Heat transfer from cylinders having closely spaced fins.
Published: (1937)

The design of airplane-engine superchargers.
Published: (1937)

Research and design problems introduced by increased power output.
Published: (1937)