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Y 3.N 21/5:6/1323
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Charts for the minimum-weight design of multiweb wings in bending / |
1 |
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Y 3.N 21/5:6/1324
|
Interaction between the spars of semimonocoque wings with cutouts / |
1 |
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Y 3.N 21/5:6/1325
|
Hydrodynamic impact loads in smooth water for a prismatic float having an angle of dead rise of 30 degrees / |
1 |
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Y 3.N 21/5:6/1326
|
Airfoil in sinusoidal motion in a pulsating stream / |
2 |
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Y 3.N 21/5:6/1327
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Wind-tunnel investigation of the effect of power and flaps on the static lateral characteristics of a single-engine low-wing airplane model / |
1 |
|
Y 3.N 21/5:6/1328
|
Calculation of compressible flows past aerodynamic shapes by use of the streamline curvature / |
1 |
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Y 3.N 21/5:6/1329
|
Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes / |
1 |
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Y 3.N 21/5:6/1330
|
Effect of critical Mach number and flutter on maximum power loading of ducted fans / |
1 |
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Y 3.N 21/5:6/1331
|
Empirical method for frequency compensation of the hot-wire anemometer / |
1 |
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Y 3.N 21/5:6/1332
|
A Rapid compression machine suitable for studying short ignition delays / |
1 |
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Y 3.N 21/5:6/1333
|
Estimation of control forces of spring-tab ailerons from wind-tunnel data / |
1 |
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Y 3.N 21/5:6/1334
|
Effects of temperature distribution and elastic properties of materials on gas-turbine-disk stresses / |
1 |
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Y 3.N 21/5:6/1335
|
The Local buckling strength of lipped Z-columns with small lip width / |
1 |
|
Y 3.N 21/5:6/1336
|
The One-dimensional theory of steady compressible fluid flow in ducts with friction and heat addition / |
1 |
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Y 3.N 21/5:6/1337
|
Effect of horizontal-tail position on the hinge moments of an unbalanced rudder in attitudes simulating spin conditions / |
1 |
|
Y 3.N 21/5:6/1338
|
Propeller-efficiency charts for light airplanes / |
1 |
|
Y 3.N 21/5:6/1339
|
Wind-tunnel investigation of the effect of power and flaps on the static longitudinal stability and control characteristics of a single-engine high-wing airplane model / |
1 |
|
Y 3.N 21/5:6/1340
|
Subsonic flow over thin oblique airfoils at zero lift / |
1 |
|
Y 3.N 21/5:6/1341
|
A Simplified method of elastic-stability analysis for thin cylindrical shells. : 1 - Donnell's equation / |
1 |
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Y 3.N 21/5:6/1342
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A Simplified method of elastic-stability analysis for thin cylindrical shells. : 2 - Modified equilibrium equation / |
1 |
