Effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data.
| Corporate Author: | United States. National Advisory Committee for Aeronautics |
|---|---|
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington] :
[s.n.],
1936.
|
| Subjects: | |
| Online Access: | Electronic resource (PDF) |
Similar Items
Comparative flight and full-scale wind℗--tunnel measurements of the maximum lift of airplane.
Published: (1937)
Published: (1937)
Experimental investigation of wind-tunnel interference on the downwash behind an airfoil.
Published: (1937)
Published: (1937)
A simplified application of the method of operators to the calculation of disturbed motions of an airplane.
Published: (1936)
Published: (1936)
Tests of related forward-camber airfoils in the variable-density wind tunnel.
Published: (1939)
Published: (1939)
Fuselage-drag tests in the variable-density wind tunnel : Streamline bodies of revolution, fineness ratio of 5.
Published: (1937)
Published: (1937)
General airplane performance.
Published: (1937)
Published: (1937)
Characteristics of 78 related airfoil sections from tests in variable℗-density wind tunnel.
Published: (1933)
Published: (1933)
Wind℗--tunnel investigation of tapered wings with ordinary ailerons and partial℗--span split flaps.
Published: (1937)
Published: (1937)
Wind℗--tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps.
Published: (1937)
Published: (1937)
R©♭sum©♭ and analysis of N. A. C. A. lateral control research.
Published: (1937)
Published: (1937)
Wind℗--tunnel interference with particular reference to off℗--center positions of wing and to downwash at tail.
Published: (1935)
Published: (1935)
Wind℗--tunnel and flight tests of slot-lip ailerons.
Published: (1937)
Published: (1937)
Forces and moments acting on parts of XN2Y-1 airplane during spins.
Published: (1936)
Published: (1936)
Flight and wind-tunnel tests of XBM-1 dive bomber.
Published: (1938)
Published: (1938)
Measurements of intensity and scale of wind-tunnel turbulence and their relation to critical Reynolds number of spheres.
Published: (1936)
Published: (1936)
Wind℗--tunnel tests of Clark Y wing having split flaps with gaps.
Published: (1938)
Published: (1938)
Air flow in the boundary layer near a plate.
Published: (1936)
Published: (1936)
Wing-nacelle℗--propeller interference for wings of various spans, force, and pressure℗--distribution tests.
Published: (1936)
Published: (1936)
Pressure distribution over airfoils with Fowler flaps.
Published: (1937)
Published: (1937)
Air propellers in yaw.
Published: (1936)
Published: (1936)
Span load distribution for tapered wings with partial℗--span flaps.
Published: (1936)
Published: (1936)
Spinning characteristics of wings IV : Changes in stagger of rectangular Clark Y biplane cellules.
Published: (1937)
Published: (1937)
Pressure-distribution measurements at large angles of pitch on fins of different span-chord ratio on a 1/40-scale model of the U. S. airship "Akron".
Published: (1937)
Published: (1937)
Calculation of induced efficiency of heavily loaded propellers having infinite number of blades; Induced efficiency of optimum propellers having finite number of blades; Prospects of propeller drive for high flying speeds.
Published: (1939)
Published: (1939)
Compressible flow about symmetrical Joukowski profiles.
Published: (1937)
Published: (1937)
Drag of cylinders of simple shapes.
Published: (1937)
Published: (1937)
An analysis of the factors that determine the periodic twist of an autogiro rotor blade, with a comparison of predicted and measured results.
Published: (1937)
Published: (1937)
Tests of a wing-nacelle-propeller combination at several pitch settings up to 42℗ʻ.
Published: (1936)
Published: (1936)
The variation with Reynolds number of pressure distribution over an airfoil section.
Published: (1938)
Published: (1938)
Comparison of profile-drag and boundary℗--layer measurements obtained in flight and in the full℗--scale wind tunnel.
Published: (1939)
Published: (1939)
Calculated and measured pressure distributions over the midspan section of the N. A. C. A. 4412 airfoil.
Published: (1936)
Published: (1936)
Theoretical study of various airplane motions after initial disturbance.
Published: (1938)
Published: (1938)
Influence of lateral stability on disturbed motions of airplane with special reference to motions produced by gusts.
Published: (1938)
Published: (1938)
Wind tunnel test of Curtiss PW-8 pursuit airplane (Airplane Section report).
Published: (1925)
Published: (1925)
Wind tunnel test of CO-2A model airplane (Airplane Section report).
Published: (1924)
Published: (1924)
Theory of automatic control of airplanes.
Published: (1939)
Published: (1939)
Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law.
Published: (1937)
Published: (1937)
Wind℗--tunnel tests of 3 lateral-control devices in combination with full℗--span slotted flap on N. A. C. A. 23012 airfoil.
Published: (1938)
Published: (1938)
Behavior of turbulent boundary layers on curved convex walls.
Published: (1936)
Published: (1936)
The effect of curvature on the transition from laminar to turbulent boundary layer.
Published: (1937)
Published: (1937)