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Y 3.N 21/5:8/1225
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Test report on three- and six-component measurements on a series of tapered wings of small aspect ratio. : (Partial Report: Trapezoidal wing) / |
1 |
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Y 3.N 21/5:8/1226
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On the installation of jet engine nacelles on a wing. : Fourth partial report: pressure-distribution measurements on a swept-back wing with jet engine nacelle / |
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Y 3.N 21/5:8/1227
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Moments of cambered round bodies / |
1 |
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Y 3.N 21/5:8/1228
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Behavior of the laminar boundary layer for periodically oscillating pressure variation / |
1 |
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Y 3.N 21/5:8/1229
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Heat transmission in the boundary layer / |
1 |
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Y 3.N 21/5:8/1230
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Effect of the acceleration of elongated bodies of revolution upon the resistance in a compressible flow / |
1 |
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Y 3.N 21/5:8/1231
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Report on investigation of developed turbulence / |
1 |
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Y 3.N 21/5:8/1233
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Contribution to the problem of flow at high speed / |
1 |
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Y 3.N 21/5:8/1234
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Computation of thin-walled prismatic shells / |
1 |
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Y 3.N 21/5:8/1235
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Investigation of conditions of titanium carbonization - IV / |
1 |
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Y 3.N 21/5:8/1236
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A class of de Laval nozzles / |
1 |
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Y 3.N 21/5:8/1237
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On the motions of an oscillating system under the influence of flip-flop controls / |
1 |
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Y 3.N 21/5:8/1238
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Two-dimensional wing theory in the supersonic range / |
1 |
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Y 3.N 21/5:8/1239
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Two-dimensional motion of a gas at large supersonic velocities / |
1 |
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Y 3.N 21/5:8/1240
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Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter) / |
1 |
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Y 3.N 21/5:8/1241
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Basic differential equations in general theory of elastic shells / |
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Y 3.N 21/5:8/1242
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Theory of characteristics / |
1 |
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Y 3.N 21/5:8/1243
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Two-dimensional potential flows / |
1 |
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Y 3.N 21/5:8/1244
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Rotationally symmetric potential flows / |
1 |
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Y 3.N 21/5:8/1245
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Lift force of an arrow-shaped wing / |
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