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Y 3.N 21/5:6/2870
|
Power-off flare-up tests of a model helicopter rotor in vertical autorotation / |
1 |
|
Y 3.N 21/5:6/2871
|
Experimental investigation of loss in an annular cascade of turbine-nozzle blades of free vortex design / |
1 |
|
Y 3.N 21/5:6/2872
|
The effect of initial curvature on the strength of an inelastic column / |
1 |
|
Y 3.N 21/5:6/2873
|
The effect of longitudinal stiffeners located on one side of a plate on the compressive buckling stress of the plate-stiffener combination / |
1 |
|
Y 3.N 21/5:6/2874
|
On traveling waves in beams / |
1 |
|
Y 3.N 21/5:6/2875
|
Behavior in pure bending of a long monocoque beam in circular-arc cross section / |
1 |
|
Y 3.N 21/5:6/2876
|
The planing characteristics of two V-shaped prismatic surfaces having angles of dead rise of 20 degrees and 40 degrees / |
1 |
|
Y 3.N 21/5:6/2877
|
On the use of a damped sine-wave elevator motion for computing the design maneuvering horizontal-tail load / |
1 |
|
Y 3.N 21/5:6/2878
|
Combined effect of damping screens and stream convergence on turbulence / |
1 |
|
Y 3.N 21/5:6/2879
|
Unsteady oblique interaction of a shock wave with a plane disturbance / |
1 |
|
Y 3.N 21/5:6/2880
|
A digital automatic multiple pressure recorder / |
1 |
|
Y 3.N 21/5:6/2881
|
Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller / |
2 |
|
Y 3.N 21/5:6/2882
|
Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system / |
1 |
|
Y 3.N 21/5:6/2883
|
Bearing strengths of some 75S-T6 and 14S-T6 aluminum-alloy hand forgings / |
1 |
|
Y 3.N 21/5:6/2884
|
Calculation and measurement of normal modes of vibration of an aluminum-alloy box beam with and without large discontinuities / |
1 |
|
Y 3.N 21/5:6/2885
|
Some exact solutions of two-dimensional flows of compressible fluid with hodograph method / |
1 |
|
Y 3.N 21/5:6/2886
|
An analysis of statically indeterminate trusses having members stressed beyond the proportional limit / |
1 |
|
Y 3.N 21/5:6/2887
|
On the stability of the laminar mixing region between two parallel streams in a gas / |
1 |
|
Y 3.N 21/5:6/2888
|
Performance characteristics of plane-wall two-dimensional diffusers / |
1 |
|
Y 3.N 21/5:6/2889
|
Estimation of hydrodynamic impact loads and pressure distributions on bodies approximating elliptical cylinders with special reference to water landings of helicopters / |
1 |
