Call Number (LC) Title Results
Y 3.N 21/5:6/1646 Low-speed wind-tunnel investigation of various plain-spoiler configurations for lateral control on a 42 degree sweptback wing / 1
Y 3.N 21/5:6/1647 Sound-level measurements of a light airplane modified to reduce noise reaching the ground / 1
Y 3.N 21/5:6/1648 Tank tests of a 1/10-size model of a hypothetical flying boat with a hull length-beam ratio of 9.0 / 1
Y 3.N 21/5:6/1649 Investigation of a 1/7-scale powered model of a twin-boom airplane and a comparison of its stability, control, and performance with those of a similar all-wing airplane / 1
Y 3.N 21/5:6/1650 Chordwise and spanwise loadings measured at low speed on a triangular wing having an aspect ratio of two and an NACA 0012 airfoil section / 1
Y 3.N 21/5:6/1651 Supersonic nozzle design / 1
Y 3.N 21/5:6/1652 Investigation of axial-flow fan and compressor rotors designed for three-dimensional flow. / 1
Y 3.N 21/5:6/1653 Charts for the computation of equilibrium composition of chemical reactions in the carbon-hydrogen-oxygen-nitrogen system at temperatures from 2000 to 5000 degrees K / 1
Y 3.N 21/5:6/1654 Sound from dual-rotating and multiple single-rotating propellers / 1
Y 3.N 21/5:6/1655 Thermodynamic charts for the computation of fuel quantity required for constant-pressure combustion with diluents / 1
Y 3.N 21/5:6/1656 Tests of six types of bakelite-bonded wire strain gages / 1
Y 3.N 21/5:6/1657 Effects of compressibility on the flow past thick airfoil sections / 1
Y 3.N 21/5:6/1658 Lateral stability and control characteristics of a free-flying model having an unsweptwing with an aspect ratio of 2 / 1
Y 3.N 21/5:6/1659 Method for calculation of pressure distribution on thin conical bodies of arbitrary cross section in supersonic stream / 1
Y 3.N 21/5:6/1660 Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds / 1
Y 3.N 21/5:6/1661 Critical axial-compressive stress of a curved rectangular panel with a central chordwise stiffner / 1
Y 3.N 21/5:6/1662 Aerodynamic properties of slender wing-body combinations at subsonic, transonic, and supersonic speeds / 2
Y 3.N 21/5:6/1663 High-speed wind-tunnel investigation of an NACA 65-210 semispan wing equipped with plug and retractable ailerons and a full-span slotted flap / 1
Y 3.N 21/5:6/1664 A Device for measuring sonic velocity and compressor Mach number / 1
Y 3.N 21/5:6/1665 Characteristics of low-aspect-ratio wings at supercritical Mach numbers / 1