|
Y 3.N 21/5:8/729
|
The flight of an autogiro at high speed / |
1 |
|
Y 3.N 21/5:8/730
|
Practical experiences with lightning discharges to airplanes / |
1 |
|
Y 3.N 21/5:8/731
|
Trend of airplane flight characteristics / |
1 |
|
Y 3.N 21/5:8/732
|
Evaluation of scavenging in two-stroke-cycle engines / |
1 |
|
Y 3.N 21/5:8/733
|
Aerodynamic principles of the direct lifting propeller / |
1 |
|
Y 3.N 21/5:8/734
|
The small wind tunnel of the DVL / |
1 |
|
Y 3.N 21/5:8/735
|
The high-speed tank of the Hamburg shipbuilding company / |
1 |
|
Y 3.N 21/5:8/736
|
Effect of fuselage and engine nacelles on some aerodynamic properties of an airplane wing / |
1 |
|
Y 3.N 21/5:8/737
|
Conversion of energy in cross-sectional divergences under different conditions of inflow / |
1 |
|
Y 3.N 21/5:8/738
|
Investigation of a Rateau supercharger for a 700-horsepower airplane engine / |
1 |
|
Y 3.N 21/5:8/739
|
Experiments with planing surfaces / |
1 |
|
Y 3.N 21/5:8/740
|
The development of floats and equipment for research in promoting it / |
1 |
|
Y 3.N 21/5:8/741
|
The calculation of lateral stability with free controls / |
1 |
|
Y 3.N 21/5:8/742
|
Supplemental data and calculations of the lateral stability of airplanes / |
1 |
|
Y 3.N 21/5:8/743
|
Fatigue strength of airplane an engine materials / |
1 |
|
Y 3.N 21/5:8/744
|
Torsional stresses in box beams with cross sections partially restrained against warping / |
1 |
|
Y 3.N 21/5:8/745
|
High-speed aircraft / |
1 |
|
Y 3.N 21/5:8/746
|
The high-speed Heinkel HE 70 mail airplane / |
1 |
|
Y 3.N 21/5:8/747
|
Analysis of spinning in a monoplane wing by the induction method as compared with the strip method / |
1 |
|
Y 3.N 21/5:8/748
|
Impact buckling of thin bars in the elastic range hinged at both ends / |
1 |
