Aeronautical Engineering for National Certificate, Τόμος 1

acceleration aerodynamic aerofoil aerofoil section aeroplane air1 aircraft airspeed airstream angle of attack applied assumed beam bending moment diagrams bolt C₁ Calculate cantilever centroid Chapter chord coefficient compression CONCENTRATED LOAD consider constant cross-sectional area curve denoted density determine diameter distance drag drag coefficient energy equal equation equilibrium example flow fluid follows force and bending forces acting frame fuselage gauge Hence hollow shaft IN.A indicated joint length lift lift forces manometer mass material maximum measure modulus moment of area monocoque NATIONAL CERTIFICATE neutral axis obtained perpendicular pitot-static tube plane plate pressure difference ratio resultant force rivet shear strain shear stress shown in Fig slugs spar speed static pressure streamline structure Taking moments tensile stress tension thickness tons per sq torque true airspeed undisturbed stream velocity volume W₁ weight wind tunnel Young's modulus zero