Call Number (LC) Title Results
Y 3.N 21/5:6/400 Advantages of oxide films as bases for aluminum pigmented surface coatings for aluminum alloys / 2
Y 3.N 21/5:6/401 Tests of N.A.C.A. airfoils in the variable density wind tunnel.
Tests of N.A.C.A. airfoils in the variable-density wind tunnel. : Series 44 and 64 / 		2
Y 3.N 21/5:6/402 The effectiveness of a double-stem injection valve in controlling combustion in a compression-ignition system /
The Effectiveness of a double-stem injection valve in controlling combustion in a compression-ignition engine / 		2
Y 3.N 21/5:6/403 The interference effects on an airfoil of a flat plate at mid-span position /
The Interference effects on an airfoil of a flate plate at mid-span position / 		2
Y 3.N 21/5:6/404 Tests of N.A.C.A. airfoils in the variable-density wind tunnel.
Tests of N.A.C.A. airfoils in the variable-density wind tunnel. : Series 24 / 		2
Y 3.N 21/5:6/405 Valve timing of engines having intake pressures higher than exhaust / 2
Y 3.N 21/5:6/406 The use of large valve overlap in scavenging a supercharged spark-ignition engine using fuel injection / 2
Y 3.N 21/5:6/407 Effect of the reservoir volume on the discharge pressures in the injection system of the N.A.C.A. spray photography equipment / 2
Y 3.N 21/5:6/408 Preliminary tests on the vaporization of fuel sprays / 2
Y 3.N 21/5:6/409 Effect of aging on taut rubber diaphragms / 2
Y 3.N 21/5:6/410 Experiments on the distribution of fuel in fuel sprays / 2
Y 3.N 21/5:6/411 Rapid chemical test for the identification of chromium-molybdenum steel aircraft tubing / 2
Y 3.N 21/5:6/412 The aerodynamic characteristics of airfoils at negative angles of attack /
The Aerodynamic characteristics of airfoils at negative angles of attack / 		2
Y 3.N 21/5:6/413 The compressive strength of duralumin columns of equal angle section /
The Compressive strength of duralumin columns of equal angle section / 		2
Y 3.N 21/5:6/414 Considerations of air flow in combustion chambers of high-speed compression-ignition engines / 2
Y 3.N 21/5:6/415 Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings / 2
Y 3.N 21/5:6/416 Characteristics of two sharp-nosed airfoils having reduced spinning tendencies / 2
Y 3.N 21/5:6/417 Wind-tunnel tests of a Hall high-lift wing / 2
Y 3.N 21/5:6/418 Compression-ignition engine tests of several fuels / 2
Y 3.N 21/5:6/419 Wind-tunnel tests of the Fowler variable-area wing / 2