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Sixteenth annual report
The Office of Aeronautical Intelligence
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aerodynamic aileron AILERON SPAN airfoil characteristics corrected airplane airship angle of attack aspect ratio average beams biplane buckling Bureau of Aeronautics Bureau of Standards cap strip CENT OF WING Committee for Aeronautics compression curves cylinder deflection density determined diagonals diameter duralumin edge effect engine equation experimental factor failure feet flap flight fuel fuselage given increase induced drag injection valve investigation joint Langley Field lift coefficient material measured metal method modulus modulus of rigidity monoplane N. A. C. A. Technical Report National Advisory Committee Navy obtained orifice pitch plate plywood pounds per square reaction Reference Reynolds Number Roots type supercharger seaplane shear shown in Figure Sitka spruce species specific gravity specimens spruce square inch strength properties stress supercharger surface Table temperature tensile tests thickness tion tube turbulence values velocity weight welding width wind tunnel wire wood yawing