Call Number (LC) Title Results
Y 3.N 21/5:6/500 The torsional stiffness of thin duralumin shells subjected to large torques / 2
Y 3.N 21/5:6/501 Landing-shock recorder / 2
Y 3.N 21/5:6/502 Aerodynamic investigation of a cup anemometer / 2
Y 3.N 21/5:6/503 Measurement of altitude in blind flying / 2
Y 3.N 21/5:6/504 Complete tank tests of two flying-boat hulls with pointed steps - N.A.C.A. Models 22-A and 35 / 2
Y 3.N 21/5:6/505 The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing / 2
Y 3.N 21/5:6/506 Experimental verification of Theodorsen's theoretical jet-boundary correction factors / 2
Y 3.N 21/5:6/507 The effects of equal-pressure fixed slots on the characteristics of a Clark Y aerofoil /
The effects of equal-pressure fixed slots on the characteristics of a Clark Y airfoil / 		2
Y 3.N 21/5:6/508 Landing characteristics of an autogiro / 2
Y 3.N 21/5:6/509 Tank tests of flat and V-bottom planing surfaces /
Tank tests of flat and v-bottom planing surfaces / 		2
Y 3.N 21/5:6/510 The calculated effect of trailing-edge flaps on the take-off of flying boats / 2
Y 3.N 21/5:6/511 A study of the pitching moments and the stability characteristics of monoplanes / 2
Y 3.N 21/5:6/512 A complete tank test of the hull of the Sikorsky S-40 flying boat - American Clipper Class /
A complete tank test on the hull of the Sikorsky S-40 flying boat - American Clipper Class / 		2
Y 3.N 21/5:6/513 The wave suppressors used in the N.A.C.A. tank / 2
Y 3.N 21/5:6/514 Effect of combustion-chamber shape on the performance of a prechamber compression-ignition engine / 2
Y 3.N 21/5:6/515 Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model / 2
Y 3.N 21/5:6/516 Propeller vibrations and the effect of the centrifugal force / 1
Y 3.N 21/5:6/517 The aerodynamic forces and moments on a spinning model of the F4B-2 airplane as measured by the spinning balance / 1
Y 3.N 21/5:6/518 Performance tests of a single-cylinder compression-ignition engine with a displacer piston / 1
Y 3.N 21/5:6/519 Vortex noise from rotating cylindrical rods / 1