Call Number (LC) Title Results
Y 3.N 21/5:6/1967 A comparison of wing loads measured in flight on a fighter-type airplane by strain-gage and pressure-distribution methods / 1
Y 3.N 21/5:6/1968 Flight tests of the hydrodynamic characteristics of a Japanese "Emily" flying boat / 1
Y 3.N 21/5:6/1969 Comparative drag measurements at transonic speeds of rectangular and sweptback NACA 65-009 airfoils mounted on a freely falling body / 1
Y 3.N 21/5:6/1970 Methods of designing cascade blades with prescribed velocity distributions in compressible potential flows / 1
Y 3.N 21/5:6/1971 Plastic buckling of extruded composite sections in compression / 1
Y 3.N 21/5:6/1972 Critical shear stress of a curved rectangular panel with a central stiffener / 1
Y 3.N 21/5:6/1973 Theoretical spanwise lift distributions of low-aspect-ratio wings at speeds below and above the speed of sound / 1
Y 3.N 21/5:6/1974 Effect of open circular holes on tensile strength and elongation of sheet specimens of some aluminum alloys / 1
Y 3.N 21/5:6/1975 Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds / 1
Y 3.N 21/5:6/1976 Summary of information relating to gust loads on airplanes / 1
Y 3.N 21/5:6/1977 Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speeds / 1
Y 3.N 21/5:6/1978 Data on the compressive strength of 75S-T6 aluminum-alloy flat panels having small, thin, widely spaced, longitudinal extruded Z-section stiffeners / 1
Y 3.N 21/5:6/1979 A radar method of calibrating airspeed installations on airplanes in maneuvers at high altitudes and at transonic and supersonic speeds / 1
Y 3.N 21/5:6/1980 Effect of forebody warp and increase in afterbody length on the hydrodynamic qualities of a flying-boat hull of high length-beam ratio / 1
Y 3.N 21/5:6/1981 Critical stress of ring-stiffened cylinders in torsion / 1
Y 3.N 21/5:6/1982 An introduction to the physical aspects of helicopter stability / 1
Y 3.N 21/5:6/1983 Longitudinal flying qualities of several single-rotor helicopters in forward flight / 1
Y 3.N 21/5:6/1984 A semiempirical method for estimating the rolling moment due to yawing of airplanes / 1
Y 3.N 21/5:6/1985 Elastic buckling of outstanding flanges clamped at one edge and reinforced by bulbs at other edge / 1
Y 3.N 21/5:6/1986 Stability of Alclad plates / 1