Y 3.N 21/5:5/793
|
Experiments on drag of revolving disks, cylinders, and streamline rods at high speeds. |
1 |
Y 3.N 21/5:5/794
|
The flow of a compressible fluid past a circular arc profile. |
1 |
Y 3.N 21/5:5/795
|
The NACA impact basin and water landing tests of a float model at various velocities and weights. |
1 |
Y 3.N 21/5:5/798
|
Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers. |
1 |
Y 3.N 21/5:5/800
|
Effects of small angles of sweep and moderate amounts of dihedral on stalling and lateral characteristics of a wing-fuselage combination equipped with partial- and full-span double slotted flaps. |
1 |
Y 3.N 21/5:5/801
|
A method for studying the hunting oscillations of an airplane with a simple type of automatic control. |
1 |
Y 3.N 21/5:5/803
|
Wind-tunnel investigation of the effects of profile modification and tabs on the characteristics of ailerons on a low-drag airfoil. |
1 |
Y 3.N 21/5:5/805
|
An analysis of life expectancy of airplane wings in normal cruising flight. |
1 |
Y 3.N 21/5:5/887
|
Critical-stress of thin-walled cylinders in axial compression / |
1 |
Y 3.N 21/5:5/934
|
Recommendations for numerical solution of reinforced-panel and fuselage-ring problems / |
1 |
Y 3.N 21/5:5/1135
|
Equations, tables, and charts for compressible flow. |
1 |
Y 3.N 21/5:6/
|
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 21/5:6/1
|
Notes on longitudinal stability and balance / |
1 |
Y 3.N 21/5:6/2
|
Airplane performance as influenced by the use of a supercharged engine / |
1 |
Y 3.N 21/5:6/3
|
Notes on the theory of the accelerometer / |
1 |
Y 3.N 21/5:6/4
|
The problem of the helicopter / |
1 |
Y 3.N 21/5:6/5
|
Relation of rib spacing to stress in wing planes / |
1 |
Y 3.N 21/5:6/6
|
Static testing and proposed standard specifications / |
1 |
Y 3.N 21/5:6/7
|
Notes on the design of supercharged and over-dimensioned aircraft engines / |
1 |
Y 3.N 21/5:6/8
|
Duralumin / |
1 |