Call Number (LC) Title Results
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
Y 3.N 21/5:6/310 Wind tunnel pressure distribution tests on a series of biplane wing models. 1
Y 3.N 21/5:6:310 Wind tunnel pressure distribution tests on a series of biplane wing models : Part 1. Effects of changes in stagger and gap / 1
Y 3.N 21/5:6/311 The use of wheel brakes on airplanes /
The Use of wheel brakes on airplanes /
2
Y 3.N 21/5:6/312 Sphere drag tests in the variable density wind tunnel / 2
Y 3.N 21/5:6/313 The formation of ice upon airplanes in flight /
The Formation of ice upon airplanes in flight /
2
Y 3.N 21/5:6/314 Spiral tendency in blind flying / 2
Y 3.N 21/5:6/315 Viscosity of diesel engine fuel oil under pressure / 2