Contributions to the theory of incomplete tension bay.
| Corporate Author: | United States. National Advisory Committee for Aeronautics |
|---|---|
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington] :
[s.n.],
1937.
|
| Subjects: | |
| Online Access: | Electronic resource (PDF) |
Similar Items
Tests for the determination of the stress condition in tension fields.
Published: (1936)
Published: (1936)
Airfoil theory at supersonic speed.
Published: (1939)
Published: (1939)
The strength of shell bodies--theory and practice.
Published: (1937)
Published: (1937)
Theory of contra-vanes applied to propeller.
Published: (1939)
Published: (1939)
On some reciprocal relations in theory of nonstationary flows.
Published: (1938)
Published: (1938)
Contribution to theory of heated duct radiator.
Published: (1939)
Published: (1939)
Contribution to the problem of airfoils spanning a free jet.
Published: (1936)
Published: (1936)
The ground effect on lifting propellers.
Published: (1937)
Published: (1937)
Aerodynamic characteristics of full℗--scale propellers having 2, 3, and 4 blades of Clark Y and R. A. F. 6 airfoil sections.
Published: (1937)
Published: (1937)
Method of curved models and its application to the study of curvilinear flight of airships, pt. 2.
Published: (1937)
Published: (1937)
The scale effect in towing tests with airplane-float systems.
Published: (1937)
Published: (1937)
Study of factors affecting range of airplanes.
Published: (1937)
Published: (1937)
Pressure distribution over Clark Y-H airfoil section with split flap.
Published: (1937)
Published: (1937)
Flight comparison of conventional ailerons on rectangular wing and of conventional and floating wing℗--tip ailerons on tapered wing.
Published: (1937)
Published: (1937)
The gyroplane--its principles and its possibilities.
Published: (1937)
Published: (1937)
Turbulent boundary layer of an airfoil.
Published: (1937)
Published: (1937)
On the actual loads on airplane landing gears.
Published: (1937)
Published: (1937)
Experimental and calculated characteristics of 22 tapered wings [aircraft].
Published: (1937)
Published: (1937)
Charts for checking the stability of plane systems of rods.
Published: (1937)
Published: (1937)
Torsion tests of tubes.
Published: (1937)
Published: (1937)
Method of curved models and its application to the study of curvilinear flight of airships, pt. 1.
Published: (1937)
Published: (1937)
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails : 1. Basic loading condition.
Published: (1937)
Published: (1937)
Transition phase in take-off of airplane.
Published: (1937)
Published: (1937)
A simplified method for the calculation of airfoil pressure distribution.
Published: (1939)
Published: (1939)
N.A.C.A. Stall-warning indicator.
Published: (1938)
Published: (1938)
Airfoil section characteristics as applied to prediction of air forces and their distribution on wings.
Published: (1938)
Published: (1938)
Effect of compressibility on 8 full-scale propellers operating in take℗--off and climbing range.
Published: (1938)
Published: (1938)
Pressure℗--distribution investigation of an N. A. C. A. 0009 airfoil with 50-percent-chord plain flap and three tabs.
Published: (1939)
Published: (1939)
Calculation of chord-wise load distribution over air℗-foil sections with plain, split, or serially hinged trailing℗--edge flaps.
Published: (1938)
Published: (1938)
An approximate spin design criterion for monoplanes.
Published: (1939)
Published: (1939)
Tests of N. A. C. A. 23012 airfoil with slotted deflector flap.
Published: (1939)
Published: (1939)
Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression.
Published: (1939)
Published: (1939)
Wind-tunnel investigation of ground effect on wings with flaps.
Published: (1939)
Published: (1939)
Tank tests of model 36 flying-boat hull.
Published: (1938)
Published: (1938)
The influence of wing setting on wing load and rotor speed of PCA-2 autogiro as determined in flight.
Published: (1934)
Published: (1934)
Wind℗--tunnel investigation of effect of yaw on lateral-stability characteristics : 1, Four N. A. C. A. 23012 wings of various plan forms with and without dihedral.
Published: (1939)
Published: (1939)
Lift distribution of wings with end plates.
Published: (1938)
Published: (1938)
Measurement of the air-flow velocity in the cylinder of an airplane engine.
Published: (1939)
Published: (1939)
Pressure distribution over N. A. C. A. 23012 airfoil with slotted and plain flap [National Advisory Committee for Aeronautics].
Published: (1938)
Published: (1938)
Effect of masses of controls on longitudinal stability with free elevator.
Published: (1939)
Published: (1939)