Call Number (LC) Title Results
Y 3.N 21/5:6/1586 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 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 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 Effect of longitudinal stiffners on the buckling load of long flat plates under shear / 1
Y 3.N 21/5:6/1590 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 Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections / 2
Y 3.N 21/5:6/1592 Compressible flow tables for air / 1
Y 3.N 21/5:6/1593 Effects of nacelle position on wing-nacelle interference / 1
Y 3.N 21/5:6/1594 Experimental investigation of the effects of concentrated weights on flutter characteristics of a straight cantilever wing / 1
Y 3.N 21/5:6/1595 Analysis of flight-performance measurements on a twisted, plywood-coverd helicopter rotor in various flight conditions / 1
Y 3.N 21/5:6/1596 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 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 Effects of ice formations on airplane performance in level cruising flight / 1
Y 3.N 21/5:6/1599 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 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 Characteristics of thin triangular wings with constant-chord full-span control surfaces at supersonic speeds / 1
Y 3.N 21/5:6/1602 Calculated performance of 12-cylinder liquid-cooled engine with exhaust-gas turbine geared to crankshaft / 1
Y 3.N 21/5:6/1603 Application of statistical methods to study of gas-turbine blade failures / 1
Y 3.N 21/5:6/1604 Standard symbols for helicopters / 1
Y 3.N 21/5:6/1605 Accuracy of airspeed measurements and flight calibration procedures / 1