Call Number (LC) Title Results
Y 3.N 21/5:6/366 Torsion in box wings / 2
Y 3.N 21/5:6/367 The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel /
The Aerodynamic characteristics of three tapered airfoils tested in the Variable Density Wind Tunnel / 		2
Y 3.N 21/5:6/368 The variation in pressure in the cabin of an airplane in flight /
The Variation in pressure in the cabin of an airplane in flight / 		2
Y 3.N 21/5:6/369 Effect of orifice length-diameter ratio on the coefficient of discharge of fuel-injection nozzles / 2
Y 3.N 21/5:6/370 Strength tests on paper cylinders in compression, bending, and shear / 2
Y 3.N 21/5:6/371 Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment /
Expression with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment / 		2
Y 3.N 21/5:6/372 Development of an impinging-jet fuel-injection valve nozzle / 2
Y 3.N 21/5:6/373 Investigation of the discharge rate of a fuel-injection system / 2
Y 3.N 21/5:6/374 Preliminary study of applied load factors in bumpy air / 2
Y 3.N 21/5:6/375 Moments of inertia of several airplanes / 2
Y 3.N 21/5:6/376 Effect of high air velocities on the distribution and penetration of a fuel spray / 2
Y 3.N 21/5:6/377 An integrating manometer for use in wind tunnel pressure distribution measurements /
An Integrating manometer for use in wind tunnel pressure distribution measurements / 		2
Y 3.N 21/5:6/378 Comparison of weights of 17ST and steel tubular structural members used in aircraft construction / 2
Y 3.N 21/5:6/379 The pressure distribution over a semicircular wing tip on a biplane in flight /
The Pressure distribution over a semicircular wing tip on a biplane in flight / 		2
Y 3.N 21/5:6/380 A suggested method for measuring turbulence /
A Suggested method for measuring turbulence / 		2
Y 3.N 21/5:6/381 Endurance and other properties at low temperatures of some alloys for aircraft use / 2
Y 3.N 21/5:6/382 Basic requirements of fuel-injection nozzles for quiescent combustion chambers / 2
Y 3.N 21/5:6/383 Metal-truss wing spars / 2
Y 3.N 21/5:6/384 The effect of injection-valve opening pressure on spray-tip penetration /
The Effect of injection-valve opening pressure on spray-tip penetration / 		2
Y 3.N 21/5:6/385 Tests of six symmetrical airfoils in the variable density wind tunnel / 2