Call Number (LC) Title Results
Y 3.N 21/5:6/290 Welding of high chromium steels / 1
Y 3.N 21/5:6/291 Gluing practice at aircraft manufacturing plants and repair stations / 2
Y 3.N 21/5:6/292 The drag of a J-5 radial air-cooled engine / 2
Y 3.N 21/5:6/293 The formation of ice upon the exposed parts of an airplane in flight /
The Formation of ice upon the exposed parts of an airplane in flight / 		2
Y 3.N 21/5:6/294 Wind tunnel force tests in wing systems through large angles of attack / 2
Y 3.N 21/5:6/295 The effect of tip shields on a horizontal tail surface / 1
Y 3.N 21/5:6/296 Bearing strength of wood under steel aircraft bolts and washers and other factors influencing fitting design / 2
Y 3.N 21/5:6/297 Preliminary report on the flat-top lift curve as a factor in control at low speed / 2
Y 3.N 21/5:6/298 The determination of several spray characteristics of a high-speed oil engine injection system with an oscilloscope / 1
Y 3.N 21/5:6/299 The effect of fillets between wings and fuselage on the drag and propulsive efficiency of an airplane /
The Effect of fillets between wings and fuselage on the drag and propulsive efficiency of an airplane / 		2
Y 3.N 21/5:6/300 The variation in pressures in the cockpit of an airplane in flight /
The Variation in pressures in the cockpit of an airplane in flight / 		2
Y 3.N 21/5:6/301 Drag and cooling with various forms of cowling for a "Whirlwind" engine in a cabin fuselage / 2
Y 3.N 21/5:6/302 A new method for the prediction of airplane performance /
A New method for the prediction of airplane performance / 		2
Y 3.N 21/5:6/303 Condensed data on the aircraft engines of the world / 1
Y 3.N 21/5:6/304 Corrosion embrittlement of duralumin.
Corrosion embrittlement of duralumin : 5. Results of weather-exposure tests / 		2
Y 3.N 21/5:6/305 Corrosion embrittlement of duralumin. 1
Y 3.N 21/5:6/306 Curves showing column strength of steel and duralumin tubing / 2
Y 3.N 21/5:6/307 Strength of tubing under combined axial and transverse loading / 1
Y 3.N 21/5:6/308 Pressure distribution on a slotted R.A.F. 31 airfoil in the variable density wind tunnel / 2
Y 3.N 21/5:6/309 Correcting engine tests for humidity / 1