|
Y 3.N 21/5:6/2504
|
Effects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degree sweptback surfaces with some reference to mutual interference / |
1 |
|
Y 3.N 21/5:6/2505
|
On the attached curved shock in front of a sharp-nosed axially symmetrical body placed in a uniform stream / |
1 |
|
Y 3.N 21/5:6/2506
|
An analytical determination of the flow behind a symmetrical curved shock in a uniform stream / |
1 |
|
Y 3.N 21/5:6/2507
|
Experimental investigation of oil film pressure distribution for misaligned plain bearings / |
1 |
|
Y 3.N 21/5:6/2508
|
Landing characteristics in waves of three dynamic models of flying boats / |
1 |
|
Y 3.N 21/5:6/2509
|
A self-synchronizing stroboscopic schlieren system of system for the study of unsteady air flows / |
1 |
|
Y 3.N 21/5:6/2510
|
Experimental values of the surface tension of supercooled water / |
1 |
|
Y 3.N 21/5:6/2511
|
Calculation of higher approximations for two-dimensional compressible flow by a simplified iteration process / |
1 |
|
Y 3.N 21/5:6/2512
|
Stresses in a two-bay noncircular cylinder under transverse loads / |
1 |
|
Y 3.N 21/5:6/2513
|
Effects of some solution treatments followed by an aging treatment on the life of small cast gas-turbine blades of a cobalt-chromium-base alloy. : 2 - Effect of selected combinations of soaking time, temperature, and cooling rate / |
1 |
|
Y 3.N 21/5:6/2514
|
Relative structural efficiencies of flat balsa-core sandwich and stiffened -panel construction / |
1 |
|
Y 3.N 21/5:6/2515
|
The linearized characteristics method and its application to practical nonlinear supersonic problems / |
1 |
|
Y 3.N 21/5:6/2516
|
A survey of creep in metals / |
1 |
|
Y 3.N 21/5:6/2517
|
An investigation of aircraft heaters. : XXXVII - Experimental determination of thermal and hydrodynamical behavior of air flowing along a flat plate containing turbulence promoters / |
1 |
|
Y 3.N 21/5:6/2518
|
Criterions for condensation-free flow in supersonic tunnels / |
1 |
|
Y 3.N 21/5:6/2519
|
A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory / |
1 |
|
Y 3.N 21/5:6/2520
|
Effects of pressure-rake design parameters on static-pressure measurement for rakes used in subsonic free jets / |
1 |
|
Y 3.N 21/5:6/2521
|
Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack / |
1 |
|
Y 3.N 21/5:6/2522
|
A Graphical method for plotting amplitude and phase angle of transfer functions of dynamic systems without factoring polynomials / |
1 |
|
Y 3.N 21/5:6/2523
|
Rotogenerative detection of corrosion currents / |
1 |
