Call Number (LC) Title Results
Y 3.N 21/5:6/1168 Some recent contributions to the study of transition and turbulent boundary layers / 1
Y 3.N 21/5:6/1169 The Effect of geometric dihedral on the aerodynamic characteristics of a 40 degrees swept-back wing of aspect ratio 3 / 1
Y 3.N 21/5:6/1170 On subsonic flows by a method of correspondence. : 1 - Methods for obtaining subsonic circulatory compressible flows about two-dimensional bodies / 1
Y 3.N 21/5:6/1171 On subsonic flows by a method of correspondence. : 2 - Application of methods to studies of flow with circulation about a circular cylinder / 1
Y 3.N 21/5:6/1172 Comparative tests on extruded 14S-T and extruded 24S-T hat-shape stiffener sections / 1
Y 3.N 21/5:6/1173 Flight measurements of internal cockpit pressures in several fighter-type airplanes / 1
Y 3.N 21/5:6/1174 The Application of high-temperature strain gages to the measurement of vibratory stresses in gas-turbine buckets / 1
Y 3.N 21/5:6/1175 Lifting-surface-theory aspect-ratio corrections to the lift and hinge-moment parameters for full-span elevators on horizontal tail surfaces / 1
Y 3.N 21/5:6/1176 Stresses around rectangular cut-outs with reinforced coaming stringers / 1
Y 3.N 21/5:6/1177 Effect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension / 1
Y 3.N 21/5:6/1178 A Flight investigation of the thermal performance of an air-heated propeller / 1
Y 3.N 21/5:6/1179 Notes on the theoretical characteristics of two-dimensional supersonic airfoils /
Notes on the theoretical characteristics of two-dimensional supersonic airfoils / 		2
Y 3.N 21/5:6/1180 Analysis of jet-propulsion engine combustion-chamber pressure losses / 1
Y 3.N 21/5:6/1181 Wing pressure-distribution measurements up to 0.866 Mach number in flight on a jet-propelled airplane / 2
Y 3.N 21/5:6/1182 A Collection of the collapse results of general tank tests of miscellaneous flying-boat-hull models /
A collection of the collapsed results of general tank tests of miscellaneous flying-boat-hull models / 		2
Y 3.N 21/5:6/1183 Theoretical lift and drag of thin triangular wings at supersonic speeds / 2
Y 3.N 21/5:6/1184 Theory of ground vibrations of a two-blade helicopter rotor on anisotropic flexible supports / 2
Y 3.N 21/5:6/1185 Application of the analogy between water flow with a free surface and two-dimensional compressible gas flow / 1
Y 3.N 21/5:6/1186 Review of an investigation of ceramic coatings for metallic turbine parts and other high-temperature applications / 1
Y 3.N 21/5:6/1187 Formulas for additional mass corrections to the moments of inertia of airplanes / 1