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Y 3.N 21/5:6/115
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The effect of longitudinal moment of inertia upon dynamic stability / |
1 |
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Y 3.N 21/5:6/116
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F-5-L Boat Seaplane comparative performance with direct drive and geared engines / |
1 |
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Y 3.N 21/5:6/117
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The synchronization of N.A.C.A. flight records / |
1 |
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Y 3.N 21/5:6/118
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F-5-L Boat Seaplane : performance characteristics / |
1 |
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Y 3.N 21/5:6/119
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The elimination of dead center in the controls of airplanes with thick sections / |
1 |
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Y 3.N 21/5:6/120
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A preliminary study of airplane performance / |
1 |
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Y 3.N 21/5:6/121
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Further information on the laws of fluid resistance / |
1 |
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Y 3.N 21/5:6/122
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The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals / |
1 |
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Y 3.N 21/5:6/123
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An optical altitude indicator for night landing / |
1 |
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Y 3.N 21/5:6/124
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Downwash of airplane wings / |
1 |
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Y 3.N 21/5:6/125
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Results of experimental flights at high altitudes with Daimler, Benz, and Maybach engines to determine mixture formation and heat utilization of fuel / |
1 |
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Y 3.N 21/5:6/126
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Absolute dimensions of Karman vortex motion / |
1 |
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Y 3.N 21/5:6/127
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The air propeller, its strength and correct shape / |
1 |
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Y 3.N 21/5:6/128
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Tests on an airplane model, AEG D I of the Allgemeine Elektricitats Gesellschaft, A-G, airplane construction section conducted at the Gőttingen Model Testing Laboratory for Aerodynamics / |
1 |
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Y 3.N 21/5:6/129
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Notes on aerodynamic forces on airship hulls / |
1 |
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Y 3.N 21/5:6/130
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Model supports and their effect on the results of wind tunnel tests / |
1 |
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Y 3.N 21/5:6/131
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Variation in the number of revolutions of air propellers / |
1 |
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Y 3.N 21/5:6/132
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The increase in dimensions of airplanes - weight, area, and loading of wings / |
1 |
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Y 3.N 21/5:6/133
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Disturbing effect of free hydrogen on fuel combustion in internal combustion engines / |
1 |
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Y 3.N 21/5:6/134
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Standardization and aerodynamics / |
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