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 |
Y 3.N 21/5:8/749
|
Impact buckling of thin bars in the elastic range for any end condition / |
1 |
Y 3.N 21/5:8/750
|
Influence of cut-outs in elevator on the static longitudinal stability and on the static elevator effect / |
1 |
Y 3.N 21/5:8/751
|
Investigation of boundary layers on an airplane wing in free flight / |
1 |
Y 3.N 21/5:8/752
|
Additional test data on static longitudinal stability / |
1 |
Y 3.N 21/5:8/753
|
Stipa monoplane with venturi fuselage / |
1 |