Y 3.N 21/5:6/1586
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Investigation of effectiveness of air-heating a hollow steel propeller for protection against icing. : 1- Unpartitioned blades / |
1 |
Y 3.N 21/5:6/1587
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Investigation of effectiveness of air-heating a hollow steel propeller for protection against icing. : 2-50-percent partitioned blades / |
1 |
Y 3.N 21/5:6/1588
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Investigation of effectiveness of air-heating a hollow steel propeller for protection against icing. : 3-25-percent partitioned blades / |
1 |
Y 3.N 21/5:6/1589
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Effect of longitudinal stiffners on the buckling load of long flat plates under shear / |
1 |
Y 3.N 21/5:6/1590
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Investigation of an approximately 0.178-chord-thick NACA 6-series-type airfoil section equipped with sealed internally balanced 0.20-chord ailerons and with a 0.05-chord tab / |
1 |
Y 3.N 21/5:6/1591
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Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections / |
2 |
Y 3.N 21/5:6/1592
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Compressible flow tables for air / |
1 |
Y 3.N 21/5:6/1593
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Effects of nacelle position on wing-nacelle interference / |
1 |
Y 3.N 21/5:6/1594
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Experimental investigation of the effects of concentrated weights on flutter characteristics of a straight cantilever wing / |
1 |
Y 3.N 21/5:6/1595
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Analysis of flight-performance measurements on a twisted, plywood-coverd helicopter rotor in various flight conditions / |
1 |
Y 3.N 21/5:6/1596
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An investigation of the section characteristics of plain unsealed ailerons on an NACA 66,1-115 airfoil section in the Langley 8-foot high-speed tunnel / |
1 |
Y 3.N 21/5:6/1597
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Analysis of the effects of boundary-layer control on the take-off performance characteristics of a liaison-type airplane / |
1 |
Y 3.N 21/5:6/1598
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Effects of ice formations on airplane performance in level cruising flight / |
1 |
Y 3.N 21/5:6/1599
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An Investigation of a thermal ice-prevention system for a cargo airplane. : 9 - the temperature of the wing leading-edge structure as established in flight / |
1 |
Y 3.N 21/5:6/1600
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Characteristics of thin triangular wings with triangular-tip control surfaces at supersonic speeds with Mach lines behind the leading edge / |
1 |
Y 3.N 21/5:6/1601
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Characteristics of thin triangular wings with constant-chord full-span control surfaces at supersonic speeds / |
1 |
Y 3.N 21/5:6/1602
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Calculated performance of 12-cylinder liquid-cooled engine with exhaust-gas turbine geared to crankshaft / |
1 |
Y 3.N 21/5:6/1603
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Application of statistical methods to study of gas-turbine blade failures / |
1 |
Y 3.N 21/5:6/1604
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Standard symbols for helicopters / |
1 |
Y 3.N 21/5:6/1605
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Accuracy of airspeed measurements and flight calibration procedures / |
1 |