Call Number (LC) Title Results
Y3.N21_5..6_1508 Provisional symbols and definitions for aircraft turbines. 1
Y3.N21_5..6_1756 Ultimate stresses developed by 24S-T and alclad 75S-T aluminum-alloy sheet in incomplete diagonal tension [Aeronautical research] 1
Y3.N21_5..6_1757 Performance of conical jet nozzles in terms of flow and velocity coefficients [Aeronautical research] 1
Y3.N21_5..6_1758 Properties of 19-9DL alloy bar stock at 1200 degrees F. [Aeronautical research] 1
Y3.N21_5..6_1759 Effects of compressibility on normal-force, pressure, and load characteristics of a tapered wing of NACA 66-series airfoil sections with split flaps [Aeronautical research] 1
Y3.N21_5..6_1760 NACA and Office of Naval Research metallurgical investigation of two large forged discs of S-590 alloy [Aeronautical research] 1
Y3.N21_5..6_1762 Control considerations for optimum power proportionment in turbine-propeller engines [Aeronautical research] 1
Y3.N21_5..6_1763 Flight investigation of a combined geared unbalancing-tab and servotab control system as used with an all-movable horizontal tail [Aeronautical research] 1
Y3.N21_5..6_1764 Influence of tail length upon the spin-recovery characteristics of a trainer-type-airplane model [Aeronautical research] 1
Y3.N21_5..6_1766 Wind-tunnel investigation of effects of tall length on the longitudinal and lateral stability characteristics of a single-propeller airplane model [Aeronautical research] 1
Y3.N21_5..6_1769 The flexible rectangular wing in roll at supersonic flight speeds [Aeronautical research] 1
Y3.N21_5..6_1770 Office of Naval Research and NACA metallurgical investigation of a large forged disc of Inconel X alloy, April 1949. 1
Y3.N21_5..6_1771 The development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers, December 1948. 1
Y3.N21_5..6_1772 Theoretical basic span loading characteristics of wings with arbitrary sweep, aspect ratio, and taper ratio, December 1948. 1
Y3.N21_5..6_1773 The effects of variations in Reynolds number between 3.0 x 10̂6 and 25.0 X 10̂6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections, December 1948. 1
Y3.N21_5..6_1774 Calculated performance of a compression-ignition engine-compressor-turbine combination based on experimental data, December 1948. 1
Y3.N21_5..6_1775 Hydrodynamic impact loads in smooth water for a prismatic float having an angle of dead rise of 40°, January 1949. 1
Y3.N21_5..6_1776 Hydrodynamic impact loads in rough water for a prismatic float having an angle of dead rise of 30°, December 1948. 1
Y3.N21_5..6_1777 Direct-reading design charts for 24S-T aluminum-alloy flat compression panels having longitudinal straight-web Y-section stiffeners, January 1949. 1
Y3.N21_5..7_931 Bibliography of Aeronautics, 1931. 1