Cooling tests of a single-row radial engine with several N. A. C. A. cowlings.
| 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
Design of N.A.C.A. cowlings for radial air℗--cooled engines.
Published: (1938)
Published: (1938)
Full-scale tests of a new type N. A. C. A. nose-slot cowling.
Published: (1936)
Published: (1936)
Mixture distribution in single℗--row radial engine.
Published: (1936)
Published: (1936)
Discharge characteristics of a double injection-valve single-pump injection system.
Published: (1937)
Published: (1937)
The pressure available for ground cooling in front of cowling of air-cooled airplane engines.
Published: (1938)
Published: (1938)
Cooling on front of air-cooled engine cylinder in conventional engine cowling.
Published: (1939)
Published: (1939)
Cooling characteristics of 2-row radial engine.
Published: (1935)
Published: (1935)
Analytical and experimental study of effect of periodic blade twist on thrust, torque, and flapping motion of autogiro rotor.
Published: (1937)
Published: (1937)
Effect of several factors on cooling of radial engine in flight.
Published: (1936)
Published: (1936)
Spinning characteristics of wings III : Rectangular and a tapered Clark Y monoplane wing with rounded tips.
Published: (1937)
Published: (1937)
Behavior of turbulent boundary layers on curved convex walls.
Published: (1936)
Published: (1936)
Forces and moments acting on parts of XN2Y-1 airplane during spins.
Published: (1936)
Published: (1936)
The effect of curvature on the transition from laminar to turbulent boundary layer.
Published: (1937)
Published: (1937)
R©♭sum©♭ of air-load data on slats and flaps.
Published: (1939)
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)
Published: (1938)
Measurement of the forces acting on gliders in towed flight.
Published: (1940)
Published: (1940)
The unsteady lift of a finite wing.
Published: (1939)
Published: (1939)
Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight.
Published: (1939)
Published: (1939)
Effect of ring type engine cowls on model of Douglas XO-14, 5-foot wind tunnel test numbers 35 (Airplane Branch report).
Published: (1931)
Published: (1931)
Tests of 5 full-scale propellers in presence of radial and liquid℗--cooled engine nacelle, including tests of 2 spinners.
Published: (1937)
Published: (1937)
R©♭sum©♭ and analysis of N. A. C. A. lateral control research.
Published: (1937)
Published: (1937)
Air flow in the boundary layer near a plate.
Published: (1936)
Published: (1936)
A simplified application of the method of operators to the calculation of disturbed motions of an airplane.
Published: (1936)
Published: (1936)
Tests of a wing-nacelle-propeller combination at several pitch settings up to 42℗ʻ.
Published: (1936)
Published: (1936)
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)
Wind℗--tunnel and flight tests of slot-lip ailerons.
Published: (1937)
Published: (1937)
Status of wing flutter.
Published: (1936)
Published: (1936)
Stress analysis of beams with shear deformation of the flanges.
Published: (1937)
Published: (1937)
Wind℗--tunnel tests of Clark Y wing having split flaps with gaps.
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)
Air flow around finned cylinders.
Published: (1936)
Published: (1936)
Observations in flight of region of stalled flow over blades of autogiro rotor.
Published: (1939)
Published: (1939)
Some aspects of stalling of modern low℗--wing monoplanes.
Published: (1938)
Published: (1938)
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)
Flight and wind-tunnel tests of XBM-1 dive bomber.
Published: (1938)
Published: (1938)
Wing-nacelle℗--propeller interference for wings of various spans, force, and pressure℗--distribution tests.
Published: (1936)
Published: (1936)
Fuselage-drag tests in the variable-density wind tunnel : Streamline bodies of revolution, fineness ratio of 5.
Published: (1937)
Published: (1937)
Pressure distribution over airfoils with Fowler flaps.
Published: (1937)
Published: (1937)
Tests of related forward-camber airfoils in the variable-density wind tunnel.
Published: (1939)
Published: (1939)
Effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data.
Published: (1936)
Published: (1936)