What people are saying - Write a review
We haven't found any reviews in the usual places.
Theoretical Correction for the Lift of Elliptic Wings
Airplane Vibration Tests as Belated to the Flutter Problem
50 other sections not shown
Other editions - View all
Aero aerodynamic Aeronautical Sciences air speed Aircraft Corporation airfoil airplane alloy altitude aluminum amplitude angle of attack applied approximately Aviation axis bending Bendix blade buckling calculated carburetor caster caster angle cent coefficient cold-rolled column Company compression constant Corp Curtiss-Wright Corp curve damper damping deflection determined Division effect elastic Engineer equation equilibrium factor flight flutter force formula frequency fuselage given Grover Loening increase indicated inertia Institute lift lift coefficient load Lockheed Aircraft Corporation material maximum metal method motion nose wheel obtained oxygen Paul Kollsman plane position pressure problem produce propeller radius ratio rotor shear shear stress sheet shimmy shown in Fig sound ray specimen sq.in stability steel stiffener strain stress structure supercharger surface tail temperature tensile tion torque torsional tube U.S. Army United Aircraft Corp velocity vertical vibration weight welding wing wood veneer York zero