Call Number (LC) Title Results
Y 3.N 21/5:6/425 Methods of visually determining the air flow around airplanes / 2
Y 3.N 21/5:6/426 Comparative performance of a Powerplus vane-type supercharger and an N.A.C.A. roots-type supercharger / 2
Y 3.N 21/5:6/427 Strength tests on thin-walled duralumin cylinders in torsion / 2
Y 3.N 21/5:6/428 Characteristics of an airfoil as affected by fabric sag / 2
Y 3.N 21/5:6/429 Heat dissipation from a finned cylinder at different fin-plane / air-stream angles / 2
Y 3.N 21/5:6/430 Effect of engine operating conditions on the vaporization of safety fuels / 2
Y 3.N 21/5:6/431 Tests on thrust augmentors for jet propulsion / 2
Y 3.N 21/5:6/432 Drag tests of 4/9-scale model engine nacelles with various cowlings / 1
Y 3.N 21/5:6/433 The pressure distribution over a standard and a modified Navy elliptical wing tip on a biplane in flight /
The Pressure distribution over a standard and a modified Navy elliptical wing tip on a biplane in flight / 		2
Y 3.N 21/5:6/434 Influence of several factors on ignition lag in a compression-ignition engine /
Influence of several factors on ignition lag in a compression-ignitiion engine / 		2
Y 3.N 21/5:6/435 The effect of clearance distribution on the performance of a compression-ignition engine with a precombustion chamber /
The Effect of clearance distribution on the performance of a compression-ignitiion engine with a precombustion chamber / 		2
Y 3.N 21/5:6/436 The effect of connecting-passage diameter on the performance of a compression-ignition engine with a precombustion chamber /
The Effect of connecting-passage diameter on the performance of a compression-ignitiion engine with a precombustion chamber / 		2
Y 3.N 21/5:6/436/2 Tests of nacelle-propeller combinations in various positions with reference to wings. 1
Y 3.N 21/5:6/437 The pressure distribution over a long elliptical wing tip on a biplane in flight /
The Pressure distribution over a long elliptical wing tip on a biplane in flight / 		2
Y 3.N 21/5:6/438 The gaseous explosive reaction at constant pressure - further data on the effect of inert gases /
The Gaseous explosive reaction at constant pressure - further data on the effect of inert gases / 		2
Y 3.N 21/5:6/439 Meteorological conditions during the formation of ice on aircraft / 2
Y 3.N 21/5:6/440 Flight tests to determine the effect of a fixed auxiliary airfoil on the lift and drag of a parasol monoplane / 2
Y 3.N 21/5:6/441 Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /
Rolling, yawing, and hinge moments produced by rectangular ailerons / 		2
Y 3.N 21/5:6/442 Jet propulsion with special reference to thrust augmentors / 2
Y 3.N 21/5:6/443 Wind-tunnel research comparing lateral control devices, particularly at high angles of attack.
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. : VII. Handley Page tip and full-span slots with ailerons and spoilers / 		2