| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:8/776 | A discussion of the several types of two-stroke-cycle engines / | 1 |
| Y 3.N 21/5:8/777 | Tests of spheres with reference to Reynolds number, turbulence, and surface roughness / | 1 |
| Y 3.N 21/5:8/778 | Method for the determination of the spanwise lift distribution / | 1 |
| Y 3.N 21/5:8/779 | Weldability of high-tensile steels from experience in airplane construction, with special reference to welding crack susceptibility / | 1 |
| Y 3.N 21/5:8/780 | Glider development in Germany : a technical survey of progress in design in Germany since 1922 / | 1 |
| Y 3.N 21/5:8/781 | Reduction of lift of a wing due to its drag / | 1 |
| Y 3.N 21/5:8/782 |
Status of wing flutter / Status of wing flutter. |
2 |
| Y 3.N 21/5:8/783 |
Analysis of 3 lowest bending frequencies of rotating propeller. Analysis of the three lowest bending frequencies of a rotating propeller / |
2 |
| Y 3.N 21/5:8/784 |
Torsion and buckling of open sections / Torsion and buckling of open sections. |
2 |
| Y 3.N 21/5:8/785 |
Methods and formulas for calculating the strength of plate and shell constructions as used in airplane design / Methods and formulas for calculating the strength of plate and shell constructions as used in airplane design. |
2 |
| Y 3.N 21/5:8/786 |
The formation of ice on airplanes / The formation of ice on airplanes. |
2 |
| Y 3.N 21/5:8/787 |
Investigations on the amount of downwash behind rectangular and elliptical wings / Investigations on the amount of downwash behind rectangular and elliptical wings. |
2 |
| Y 3.N 21/5:8/788 |
The 5- by 7-meter wind tunnel of the DVL. The 5- by 7- meter wind tunnel of the DVL / |
2 |
| Y 3.N 21/5:8/789 |
Turbulent jet expansion / Turbulent jet expansion. |
2 |
| Y 3.N 21/5:8/790 |
Ignition and flame development in the case of diesel fuel injection. Ignition and flame development in the case of diesel fuel injection / |
2 |
| Y 3.N 21/5:8/791 |
Behavior of turbulent boundary layers on curved convex walls / Behavior of turbulent boundary layers on curved convex walls. |
2 |
| Y 3.N 21/5:8/792 |
General instability criterion of laminar velocity distributions / General instability criterion of laminar velocity distributions. |
2 |
| Y 3.N 21/5:8/793 |
Bending of beams of thin sections / Bending of beams of thin sections. |
2 |
| Y 3.N 21/5:8/794 |
Chief characteristics and advantages of tailless airplanes / Chief characteristics and advantages of tailless airplanes. |
2 |
| Y 3.N 21/5:8/795 |
Similitude in hydrodynamic tests involving planing / Similitude in hydrodynamic tests involving planing. |
2 |
