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Comparison between theory and experiment
Dimensions of model and nomenclature
10 other sections not shown
accelerometer accuracy aerodynamic aerofoil aeroplane ailerons angular acceleration Appendix applied approximately barium chromate bending calculated cantilever cent centre chord chromate pigments CN CN CN coefficient complete cylinder compressive constant construction corresponding corrosion cross-section curvature curves cutaway damping displacement distance downstream downwash duralumin elastic elevator enamelling schemes equation flaps flexible walls flexural flutter speed formulae frequency fuselage Galerkin method ground effect inches increase inertia length lift lift coefficient longitudinal maximum measured monocoque obtained ooooooooo oscillation panel test pitching pitching moments plate polar inertia position radius ratio Rayleigh's principle reference station Reports and Memoranda ring root root chord shear stress sheet shown in Fig skin solution span stall stiffness stress distribution structure tail plane tailplane tapered theoretical theory thickness torsional tube tubular stringers uniform values velocity webs width wind tunnel zero zinc chromate