Cover Image

Effects of elevator nose shape, gap, balance, and tabs on aerodynamic characteristics of horizontal tail surface.

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

Similar Items

Notes on calculation of minimum horizontal tail surface for airplanes equipped with wing flaps.
Published: (1937)

Reduction of hinge moments of airplane control surfaces by tabs.
Published: (1935)

Effect of changes in tail arrangement upon spinning of low-wing monoplane model.
Published: (1936)

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

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

Wing-Fuselage, Interference, Tail Buffeting, and Air Flow.
Published: (1933)

Method of estimating aerodynamic effects of ordinary and split flaps of airfoils.
Published: (1936)

Calculation of aerodynamic characteristics of tapered wings with partial-span flaps.
Published: (1939)

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

Aerodynamic characteristics of 6 full-scale propellers having different airfoil sections.
Published: (1938)

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

Aerodynamic analysis of autogiro rotor with comparison between calculated and experimental results.
Published: (1934)

The Mean Aerodynamic Chord and the Aerodynamic Center of a Tapered Wing.
Published: (1945)

Effect of masses of controls on longitudinal stability with free elevator.
Published: (1939)

Free℗--spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails : 4, Effect of center-of℗--gravity location.
Published: (1939)

Interference of tail surfaces and wing and fuselage from tests of 17 combinations in N. A. C. A. variable-density tunnel.
Published: (1938)

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

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

Aerodynamics of the Fuselage.
Published: (1942)

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

Determination of Control-Surface Characteristics from NACA Plain-Flap and Tab Data.
Published: (1941)

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

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

Vibration response of airplane structures.
Published: (1934)

Effect of spray strips on take℗--off performance of model of flying-boat hull.
Published: (1934)

Tank tests of two models of flying-boat hulls to determine effect of ventilating the step.
Published: (1937)

Influence of tip shape on wing load distribution as determined by flight tests.
Published: (1934)

Considerations of the take-off problem.
Published: (1936)

Tank tests of models of flying boat hulls having longitudinal steps.
Published: (1936)

Piloting technique for recovery from spins.
Published: (1936)

Charts expressing time, velocity, and altitude relations for airplane diving in standard atmosphere.
Published: (1937)

Tank tests of model of NC flying-boat hull, N. A. C. A. model 44.
Published: (1936)

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

Measurement of true dynamic and static pressures in flight.
Published: (1939)

Notes on technique of landing airplanes equipped with wing flaps.
Published: (1936)

Tests of 16 related airfoils at high speeds.
Published: (1934)

Load tests on stiffened circular cylindrical shell.
Published: (1938)

Limitations of pilot in applying forces to airplane controls.
Published: (1936)

Calculated effect of various types of flap on take-off over obstacles.
Published: (1936)

Further measurements of normal accelerations on racing airplanes.
Published: (1936)