|
Y 3.N 21/5:6/2284
|
Lift, pitching moment, and span load characteristics of wings at low speed as affected by variations of sweep and aspect ratio / |
1 |
|
Y 3.N 21/5:6/2285
|
Damping in roll of cruciform and some related delta wings at supersonic speeds / |
1 |
|
Y 3.N 21/5:6/2286
|
Preliminary investigation of a new type of supersonic inlet / |
1 |
|
Y 3.N 21/5:6/2287
|
An investigation of pure bending in the plastic range when loads are not parallel to a principal plane / |
1 |
|
Y 3.N 21/5:6/2288
|
Estimation of low-speed lift and hinge-moment parameters for full-span trailing-edge flaps on lifting surfaces with and without sweepback / |
1 |
|
Y 3.N 21/5:6/2289
|
Elastic constants for corrugated-core sandwich plates / |
1 |
|
Y 3.N 21/5:6/2290
|
A method for calculating stresses in torsion-box covers with cutouts / |
1 |
|
Y 3.N 21/5:6/2291
|
Influence of wall boundary layer upon the performance of an axial-flow fan rotor / |
1 |
|
Y 3.N 21/5:6/2292
|
Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5 / |
1 |
|
Y 3.N 21/5:6/2293
|
The physical properties of active nitrogen in low-density flow / |
1 |
|
Y 3.N 21/5:6/2294
|
Lift and pitching derivatives of thin sweptback tapered wings with streamwise tips and subsonic leading edges at supersonic speeds / |
1 |
|
Y 3.N 21/5:6/2295
|
Chordwise and compressibility corrections to slender-wing theory / |
1 |
|
Y 3.N 21/5:6/2296
|
Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow / |
1 |
|
Y 3.N 21/5:6/2297
|
Effect of an increase in angle of dead rise on the hydrodynamic characteristics of a high-length-beam-ratio hull / |
1 |
|
Y 3.N 21/5:6/2298
|
A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution / |
1 |
|
y 3.N 21/5:6/2299
|
Exposure tests of galvanized-steel-stitched aluminum alloys / |
1 |
|
Y 3.N 21/5:6/2300
|
Analytical and experimental investigation of effect of twist on vibrations of cantilever beams / |
1 |
|
Y 3.N 21/5:6/2301
|
Linearized solution and general plastic behavior of thin plate with circular hole in strain-hardening range / |
1 |
|
Y 3.N 21/5:6/2302
|
A general through-flow theory of fluid flow with subsonic or supersonic velocity in turbomachines of arbitrary hub and casing shapes / |
1 |
|
Y 3.N 21/5:6/2303
|
Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds / |
1 |
