Cover Image

Electrical thermometers for aircraft.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1936.
Subjects:	Measuring instruments. Aeronautics > Research. Airplanes. Aerodynamics.
Online Access:	Electronic resource (PDF)

Similar Items

Aircraft rate℗--of-climb indicators.
Published: (1939)

An instrument for estimating tautness of doped fabrics on aircraft.
Published: (1939)

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

Forces and moments acting on parts of XN2Y-1 airplane during spins.
Published: (1936)

The effect of curvature on the transition from laminar to turbulent boundary layer.
Published: (1937)

R©♭sum©♭ of air-load data on slats and flaps.
Published: (1939)

Spinning characteristics of wings III : Rectangular and a tapered Clark Y monoplane wing with rounded tips.
Published: (1937)

Corrugated metal diaphragms for aircraft pressure℗--measuring instruments.
Published: (1939)

Rate℗--of-climb recorder.
Published: (1938)

Pressure distribution on a wing section with slotted flap in free flight tests.
Published: (1937)

The Design of Propeller Blade Roots.
Published: (1942)

Sound pressure-level meter without amplification.
Published: (1937)

The critical velocity of a body towed by a cable from an airplane.
Published: (1937)

Status of wing flutter.
Published: (1936)

Stress analysis of beams with shear deformation of the flanges.
Published: (1937)

Wind℗--tunnel tests of Clark Y wing having split flaps with gaps.
Published: (1938)

Observations in flight of region of stalled flow over blades of autogiro rotor.
Published: (1939)

Some aspects of stalling of modern low℗--wing monoplanes.
Published: (1938)

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

Statistical Analysis of Service Stresses on Aircraft Wings.
Published: (1942)

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

Statistical Analysis of the Time and Fatigue Strength of Aircraft Wing Structures.
Published: (1941)

Cooling tests of a single-row radial engine with several N. A. C. A. cowlings.
Published: (1936)

Air flow around finned cylinders.
Published: (1936)

Full-scale tests of a new type N. A. C. A. nose-slot cowling.
Published: (1936)

Wind℗--tunnel and flight tests of slot-lip ailerons.
Published: (1937)

Comparison of profile-drag and boundary℗--layer measurements obtained in flight and in the full℗--scale wind tunnel.
Published: (1939)

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

Hydrodynamic and aerodynamic tests of models of floats for single℗--float seaplanes. N. A. C. A. models 41-D. 41-E. 61-A. 73 and 73-A.
Published: (1938)

Analytical and experimental study of effect of periodic blade twist on thrust, torque, and flapping motion of autogiro rotor.
Published: (1937)

Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight.
Published: (1939)

Air flow in the boundary layer near a plate.
Published: (1936)

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

Effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data.
Published: (1936)

Air propellers in yaw.
Published: (1936)

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

A simplified application of the method of operators to the calculation of disturbed motions of an airplane.
Published: (1936)

Tests of a wing-nacelle-propeller combination at several pitch settings up to 42℗ʻ.
Published: (1936)

Fuselage-drag tests in the variable-density wind tunnel : Streamline bodies of revolution, fineness ratio of 5.
Published: (1937)

Pressure distribution over airfoils with Fowler flaps.
Published: (1937)