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FEBRUARY 1946 NUMBER
JANUARY 1946 NUMBER
APRIL 1946 NUMBER
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adhesion aerodynamic Aeronautical Sciences aileron aircraft airfoil airplane altitude amplitude analysis angle applied approximately assumed atomic axial compressor beam bend blade British Thomson-Houston buckling load calculated cent centrifugal compressor chamber column combustion compression considered constant corresponding critical cylinder damping deflection determined drag drag coefficient ducted fan dynamic effect elastic energy engine factor flapping flow force formula frequency gas turbine given increase indicated inertia instability intake iterative jet engine jet propulsion lift coefficient material maximum method Metropolitan-Vickers modulus neutrons obtained panels parameters plane plate Power Jets pressure problem propeller protons ratio Reynolds Number rotor Royal Aircraft Establishment semimonocoque servo shown in Fig Silane solution specimen sq.in stability equation stalling speed static strain stress stress-strain curve stringers structure surface Table temperature theoretical theory thickness thrust tion variation velocity weight width wing zero