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Y 3.N 21/5:6/1804
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Effect of longitudinal steps on skipping characteristics of PB2Y-6 flying boat / |
1 |
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Y 3.N 21/5:6/1805
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Remarks concerning the behavior of the laminar boundary layer in compressible flows / |
1 |
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Y 3.N 21/5:6/1806
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Determination of plate compressive strengths at elevated temperatures / |
1 |
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Y 3.N 21/5:6/1807
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Effects of partial admission on performance of a gas turbine / |
1 |
|
Y 3.N 21/5:6/1808
|
Method for evaluating from shadow or schlieren photographs the pressure drag in two-dimensional or axially symmetrical flow phenomena with detached shock / |
1 |
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Y 3.N 21/5:6/1809
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The Method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack / |
1 |
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Y 3.N 21/5:6/1810
|
Comparison between predicted and observed performance of gas-turbine stator blade design for free-vortex flow / |
1 |
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Y 3.N 21/5:6/1811
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The Longitudinal stability of elastic swept wings at supersonic speed / |
1 |
|
Y 3.N 21/5:6/1812
|
The application of airfoil studies to helicopter rotor design / |
1 |
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Y 3.N 21/5:6/1813
|
A Study of flow changes associated with airfoil section drag rise at supercritical speeds / |
1 |
|
Y 3.N 21/5:6/1814
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Effects of several design variables on turbine-wheel weight / |
1 |
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Y 3.N 21/5:6/1815
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On Compressibility corrections for subsonic flow over bodies of revolution / |
1 |
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Y 3.N 21/5:6/1816
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Triangular wings cambered and twisted to support specified distributions of lift at supersonic speeds / |
1 |
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Y 3.N 21/5:6/1817
|
Plastic buckling of simply supported compressed plates / |
2 |
|
Y 3.N 21/5:6/1818
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Effect of automatic stabilization on the lateral oscillatory stability of a hypothetical airplane at supersonic speeds / |
1 |
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Y 3.N 21/5:6/1819
|
The Response of pressure measuring systems to oscillating pressures / |
1 |
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Y 3.N 21/5:6/1820
|
Strength analysis of stiffened thick beam webs / |
1 |
|
Y 3.N 21/5:6/1821
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Ambient pressure determination at high altitudes by use of free-molecule theory / |
2 |
|
Y 3.N 21/5:6/1822
|
Elastic and plastic buckling of simply supported Metalite type sandwich plates in compression / |
1 |
|
Y 3.N 21/5:6/1823
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The Buckling of parallel simply supported tension and compression members connected by elastic deflectional springs / |
1 |
