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Y 3.N 21/5:6/3027
|
Influence of rotor-engine torsional oscillation on control of gas-turbine engine geared to helicopter rotor / |
1 |
|
Y 3.N 21/5:6/3028
|
The compressible laminar boundary layer with heat transfer and small pressure gradient / |
1 |
|
Y 3.N 21/5:6/3029
|
A fundamental investigation of fretting corrosion / |
1 |
|
Y 3.N 21/5:6/3030
|
A method for calculating the subsonic steady-state loading on an airplane with a wing of arbitrary plan form and stiffness / |
1 |
|
Y 3.N 21/5:6/3031
|
Preliminary experimental investigation of low-speed turbulent boundary layers in adverse pressure gradients / |
1 |
|
Y 3.N 21/5:6/3032
|
An analytical study of the effect of airplane wake on the lateral dispersion of aerial sprays / |
1 |
|
Y 3.N 21/5:6/3033
|
Application of an electro-optical two-color pyrometer to measurement of flame temperature for liquid oxygen - hydrocarbon propellant combination / |
1 |
|
Y 3.N 21/5:6/3034
|
Graphical solution of some automatic-control problems involving saturation effects with application to yaw dampers for aircraft / |
1 |
|
Y 3.N 21/5:6/3035
|
A preliminary study of the problem of designing high-speed airplanes with satisfactory inherent damping of the Dutch roll oscillation / |
1 |
|
Y 3.N 21/5:6/3036
|
The flow about a section of a finite-aspect-ratio NACA 0015 airfoil on a transonic bump / |
1 |
|
Y 3.N 21/5:6/3037
|
Counting methods and equipment for mean-value measurements in turbulence research / |
1 |
|
Y 3.N 21/5:6/3038
|
Low-speed drag of cylinders of various shapes / |
1 |
|
Y 3.N 21/5:6/3039
|
Experimental stress analysis of stiffened cylinders with cutouts. : Pure torsion / |
1 |
|
Y 3.N 21/5:6/3040
|
Use of two-dimensional data in estimating loads on a 45 degree sweptback wing with slats and partial-span flaps / |
1 |
|
Y 3.N 21/5:6/3041
|
Summary of revised gust-velocity data obtained from V-G records taken on civil transport airplanes from 1933 to 1950 / |
1 |
|
Y 3.N 21/5:6/3042
|
High-frequency pressure indicators for aerodynamic problems / |
1 |
|
Y 3.N 21/5:6/3043
|
Application of silver chloride in investigations of elasto-plastic states of stress / |
1 |
|
Y 3.N 21/5:6/3044
|
Effect of a rapid blade-pitch increase on the thrust and induced-velocity response of a full-scale helicopter rotor / |
1 |
|
Y 3.N 21/5:6/3045
|
Analogy between mass and heat transfer with turbulent flow / |
2 |
|
Y 3.N 21/5:6/3046
|
Theoretical calculations of the effects of finite sideslip at supersonic speeds on the span loading and rolling moment for families of thin sweptback tapered wings at an angle of attack / |
1 |
