Call Number (LC) Title Results
Y 3.N 21/5:6/203 A short method of calculating torsional stresses in an airplane fuselage / 1
Y 3.N 21/5:6/204 A study of static stability of airships / 1
Y 3.N 21/5:6/205 The logarithmic polar curve - its theory and application to the predetermination of airplane performance / 1
Y 3.N 21/5:6/206 Structural weight of aircraft as affected by the system of design / 2
Y 3.N 21/5:6/207 The simplifying assumptions, reducing the strict application of classical hydrodynamics to practical aeronautical computations / 1
Y 3.N 21/5:6/208 Tests on Duralumin columns for aircraft construction /
Tests on duralumin columns for aircraft construction / 		2
Y 3.N 21/5:6/209 Tests of rotating cylinders / 2
Y 3.N 21/5:6/210 The testing of aviation engines under approximate altitude conditions / 1
Y 3.N 21/5:6/211 Aircraft engine design / 1
Y 3.N 21/5:6/212 Simplified propeller design for low-powered airplanes / 1
Y 3.N 21/5:6/213 Discharge characteristics of a high speed fuel injection engine / 1
Y 3.N 21/5:6/214 Note on the Katzmayr effect on airfoil drag / 1
Y 3.N 21/5:6/215 The calculation of wing float displacement in single-float seaplanes / 1
Y 3.N 21/5:6/216 The velocity distribution caused by an airplane at the points of a vertical plane containing the span / 1
Y 3.N 21/5:6/217 Note on the air forces on a wing caused by pitching / 1
Y 3.N 21/5:6/218 The estimation of airplane performance from wind tunnel tests on conventional airplane models / 1
Y 3.N 21/5:6/219 The comparison of well-known and new wing sections tested in the variable density wind tunnel / 2
Y 3.N 21/5:6/220 The drift of an aircraft guided towards its destination by directional receiving of radio signals transmitted from the ground / 1
Y 3.N 21/5:6/221 Model tests on the economy and effectiveness of helicopter propellers / 1
Y 3.N 21/5:6/223 Determination of the lift and drag characteristics of an airplane in flight / 1