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aerodynamical aerofoil centre aeroplane aircraft angle of incidence Appendix applied beams bending-moment calculated cent centre of gravity centre of pressure component compression Concentrated Load consideration dashpot denotes determined diagram duralumin end load engine-mounting Euler's formula eyebars factor of safety failing load feet per second fin and rudder forces front and rear front truss fuselage Hence incidence wires increased inertia interplane struts landing stroke length lift wires lift-wire Load-factor on main longeron machine main planes maximum metal spars moment of inertia normal flight obtained offset oleo original strut pin-jointed piston plane and elevators plate strut formulas portion pull rear spars rear truss ribs rivets rubber shear shear stress shown in Figs specified spruce square inch tail plane tail skid tail unit terminal velocity thrust torque total weight ultimate strength undercarriage usually velocity vertical speed yield stress Young's modulus