Call Number (LC) Title Results
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
Y 3.N 21/5:6/520 Calculations of the effect of wing twist on the air forces acting on a monoplane wing / 1
Y 3.N 21/5:6/521 Full-scale force and pressure-distribution tests on a tapered U.S.A. 45 airfoil / 1
Y 3.N 21/5:6/522 Tank tests of a model of a flying-boat hull with a fluted bottom / 1
Y 3.N 21/5:6/523 Strength tests of thin-walled duralumin cylinders in combined transverse shear and bending / 1
Y 3.N 21/5:6/524 Wind-tunnel tests of a wing with a trailing-edge auxiliary airfoil used as a flap / 1
Y 3.N 21/5:6/525 The aerodynamic drag of flying-boat hull models as measured in the N.A.C.A. 20-foot wind tunnel. 1
Y 3.N 21/5:6/526 Spinning characteristics of wings. 25 percent stagger ; 0 degree decalage ; gap/chord 1.0 / 1
Y 3.N 21/5:6/527 Strength tests of thin-walled duralumin cylinders of elliptic section / 1
Y 3.N 21/5:6/528 Wind-tunnel tests of a cyclogiro rotor / 1
Y 3.N 21/5:6/529 Analysis of a strut with a single elastic support in the span, with applications to the design of airplane jury-strut systems / 1
Y 3.N 21/5:6/530 Bending stresses due to torsion in cantilever box beams / 1