Technical Report of the Aeronautical Research Committee for the Year ..., Volume 2H.M. Stationery Office, 1931 - Aeronautics |
Contents
Members of the Committee X | 728 |
Aerodynamics | 741 |
iv Performance of a compression ignition unit with reduced | 1123 |
Copyright | |
16 other sections not shown
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Common terms and phrases
aerofoil aeroplane aileron aircraft airscrew alloy aluminium angles of incidence angular apparatus aspect ratio auxiliary aerofoil axis b₂ benzole Brinell Bristol Fighter bulb calculated castor oil cent centre chord coefficient combustion compression ratio constant CONTROL ANGLES control column corresponding crankshaft curves cylinder DEGREES/SEC density diagram diameter effect engine equation exhaust pressure experimental experiments fatigue limit flowmeter fuel full scale heat hinge ignition temperature increase indicated intake lift lift coefficient lubricating Malby & Sons maximum measured method mixture motion normal observed obtained oil gas oscillation petrol pilot planes piston PITCH plate plotted position radiator range rolling rolling moment roots rotation rudder SECONDS servo shear stress shown in Fig shows slots specimen speed stability stall stalled flight steam surface thorium torque torsiograms TORSIOGRAPH TESTS torsional Trace twin bands twinning planes unslotted velocity vibration wire zero