Experimental and analytical investigation of monocoque wing model loaded in bending.
| Corporate Author: | United States. National Advisory Committee for Aeronautics |
|---|---|
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington] :
[s.n.],
1939.
|
| Subjects: | |
| Online Access: | Electronic resource (PDF) |
Similar Items
The influence of wing setting on wing load and rotor speed of PCA-2 autogiro as determined in flight.
Published: (1934)
Published: (1934)
Experimental and calculated characteristics of 22 tapered wings [aircraft].
Published: (1937)
Published: (1937)
Statics of Circular Stiffeners for Monocoque Fuselages.
Published: (1942)
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)
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)
Wind-tunnel investigation of ground effect on wings with flaps.
Published: (1939)
Published: (1939)
Spinning characteristics of wings : 5, N. A. C. A. 0009, 23018, and 6718 monoplane wings.
Published: (1938)
Published: (1938)
Effect of slipstream on airplane wing.
Published: (1939)
Published: (1939)
Crinkling strength and bending strength of round aircraft tubing.
Published: (1938)
Published: (1938)
Lift distribution of wings with end plates.
Published: (1938)
Published: (1938)
Frequencies of cantilever wings in beam and torsional vibrations.
Published: (1940)
Published: (1940)
On the actual loads on airplane landing gears.
Published: (1937)
Published: (1937)
Effects of some common surface irregularities on wing drag.
Published: (1939)
Published: (1939)
The effects of surface waviness and of rib stitching on wing drag.
Published: (1939)
Published: (1939)
Airfoil section characteristics as applied to prediction of air forces and their distribution on wings.
Published: (1938)
Published: (1938)
Theoretical stability and control characteristics of wings with various amounts of taper and twist.
Published: (1938)
Published: (1938)
Model experiments on forces and moments acting on end plate fitted to wing.
Published: (1938)
Published: (1938)
The question of spontaneous wing oscillations (determination of critical velocity through flight-oscillation tests).
Published: (1936)
Published: (1936)
Aerodynamic characteristics of wings with cambered external-airfoil flaps, including lateral control with full-span flap.
Published: (1935)
Published: (1935)
Wind℗--tunnel investigation of effect of yaw on lateral℗--stability characteristics, II--Rectangular N. A. C. A. 23012 wing with a circular fuselage and fin.
Published: (1939)
Published: (1939)
Interference of wing and fuselage from tests of 209 combinations in N. A. C. A. variable-density tunnel.
Published: (1935)
Published: (1935)
Wind℗--tunnel tests of several forms of fixed wing slot in combination with slotted flap on N. A. C. A. 23012 airfoil.
Published: (1939)
Published: (1939)
The effects of partial℗--span slotted flaps on aerodynamic characteristics of a rectangular and a tapered N. A. C. A. 23012 wing.
Published: (1939)
Published: (1939)
Interference of wing and fuselage from tests of 18 combinations in N. A. C. A. variable-density tunnel combinations with split flap.
Published: (1938)
Published: (1938)
Influence of tip shape on wing load distribution as determined by flight tests.
Published: (1934)
Published: (1934)
Calculation of chord-wise load distribution over air℗-foil sections with plain, split, or serially hinged trailing℗--edge flaps.
Published: (1938)
Published: (1938)
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)
Relative loading on biplane wings of unequal chords.
Published: (1934)
Published: (1934)
Full-scale span load distribution on tapered wing with split flaps of various spans.
Published: (1937)
Published: (1937)
Fatigue testing of wing beams by resonance method.
Published: (1938)
Published: (1938)
A study of unsymmetrical-loading conditions.
Published: (1940)
Published: (1940)
Investigation of the prevention of ice on the airplane windshield.
Published: (1940)
Published: (1940)
Effect of Wing Loading, Aspect Ratio, and Span Loading on Flight Performances.
Published: (1940)
Published: (1940)
Chordwise Load Distrubution of Simple Rectangular Wing.
Published: (1940)
Published: (1940)
Experiments on a slotted wing.
Published: (1939)
Published: (1939)
Preliminary investigation of boundary℗--layer transition along flat plate with adverse pressure gradient.
Published: (1938)
Published: (1938)
Spinning characteristics of wings III : Rectangular and a tapered Clark Y monoplane wing with rounded tips.
Published: (1937)
Published: (1937)
Ice formation on wings.
Published: (1939)
Published: (1939)
Wind-tunnel investigation of an N. A. C. A. 23030 airfoil with various arrangements of slotted flaps.
Published: (1940)
Published: (1940)
Investigations on the amount of downwash behind rectangular and elliptical wings.
Published: (1936)
Published: (1936)