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Y 3.N 21/5:6/1676
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Graphical method of obtaining theoretical lift distributions on thin wings at supersonic speeds / |
1 |
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Y 3.N 21/5:6/1677
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Experimental and calculated characteristics of several high-aspect-ratio tapered wings incorporated NACA 44-series, 230-series, and low-drag 64-series airfoil sections / |
1 |
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Y 3.N 21/5:6/1678
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Theoretical wave drag and lift of thin supersonic ring airfoils / |
1 |
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Y 3.N 21/5:6/1679
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Flight measurements of the longitudinal stability, stalling, and lift characteristics of an airplane having a 35 degree sweptback wing without slots and with 40-percent-span slots and a comparison with wind-tunnel data / |
1 |
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Y 3.N 21/5:6/1680
|
Divergence of swept wings / |
1 |
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Y 3.N 21/5:6/1681
|
Critical shear stress of an infinitely long plate in the plastic region / |
1 |
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Y 3.N 21/5:6/1682
|
Heat transfer to bodies traveling at high speed in the upper atmosphere / |
1 |
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Y 3.N 21/5:6/1683
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An Experimental investigation of an NACA 63₁-012 airfoil section with leading edge suction slots / |
1 |
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Y 3.N 21/5:6/1684
|
A Preliminary evaluation of the use of ground radar for the avoidance of turbulent clouds / |
1 |
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Y 3.N 21/5:6/1685
|
Linearized supersonic theory of conical wings / |
1 |
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Y 3.N 21/5:6/1686
|
Effect of length-beam ratio on aerodynamic characteristics of flying-boat hulls without wing interference / |
1 |
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Y 3.N 21/5:6/1687
|
Jet diffuser for simulating ram-pressure and altitude conditions on a turbojet-engine static test stand / |
1 |
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Y 3.N 21/5:6/1688
|
Dynamometer-stand investigation of the muffler used in the demonstration of light-airplane noise reduction / |
1 |
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Y 3.N 21/5:6/1689
|
Load distributions due to steady roll and pitch for thin wings at supersonic speeds / |
1 |
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Y 3.N 21/5:6/1690
|
Theoretical and experimental wing-tip accelerations of a small flying boat during landing impacts / |
1 |
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Y 3.N 21/5:6/1691
|
Icing and de-icing of a propeller with internal electric blade heaters / |
1 |
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Y 3.N 21/5:6/1692
|
Determination of bending moments in pressure-loaded rings of arbitrary shape when deflections are considered / |
1 |
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Y 3.N 21/5:6/1693
|
An Analysis of the airspeeds and normal accelerations of Martin M-130 airplanes in commercial transport operation / |
1 |
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Y 3.N 21/5:6/1694
|
Analysis of planing data for use in predicting hydrodynamic impact loads / |
1 |
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Y 3.N 21/5:6/1695
|
Effect of pressure recovery on the performance of a jet-propelled airplane / |
1 |
