Call Number (LC) Title Results
Y 3.N 21/5:11/L288 Wind-tunnel investigation of an NACA full-span high-lift lateral-control combination. : 1 - Section characteristics, NACA 23012 airfoil / 1
Y 3.N 21/5:11/L289 Effect of changes in aileron rigging on the stick forces of a high-speed fighter airplane / 1
Y 3.N 21/5:11/L29 Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades / 1
Y 3.N 21/5:11/L290 Wind-tunnel investigation of control-surface characteristics. : 14 - NACA 0009 airfoil with a 20-percent-chord double plain flap / 1
Y 3.N 21/5:11/L291 Time-velocity-altitude relations for an airplane diving in a standard atmosphere / 1
Y 3.N 21/5:11/L292 Effects of a simulated ice formation on the aerodynamic characteristics of an airfoil / 1
Y 3.N 21/5:11/L293 Tests of hydraulically expanded rivets / 1
Y 3.N 21/5:11/L294 A study of the tightness and flushness of machine-countersunk rivets for aircraft / 1
Y 3.N 21/5:11/L295 Wind-tunnel tests of a twin-engine model to determine the effect of direction of propeller rotation on the static-stability characteristics / 1
Y 3.N 21/5:11/L296 Tapered wings, tip stalling, and preliminary results from tests of the stall-control flap / 1
Y 3.N 21/5:11/L297 Comparative tests of the strength and tightness of commercial flush rivets of one type and NACA flush rivets in machine-countersunk and counterpunched joints / 1
Y 3.N 21/5:11/L298 Use of stagnation temperature in calculating rate of heat transfer in aircraft heat exchangers / 1
Y 3.N 21/5:11/L299 Lift and drag data for 30 pusher-propeller shaft housings on an NACA 65,3-018 airfoil section / 1
Y 3.N 21/5:11/L3 A method for determining oil-cooler performance requirements in series operation / 1
Y 3.N 21/5:11/L30 The use of geared spring tabs for elevator control / 1
Y 3.N 21/5:11/L301 Wind-tunnel investigated of control-surface characteristics. : 3 - A small aerodynamic balance of various nose shapes used with a 30-percent-chord flap on an NACA 0009 airfoil / 1
Y 3.N 21/5:11/L302 A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls / 1
Y 3.N 21/5:11/L303 Test of a dual-rotation axial-flow fan / 1
Y 3.N 21/5:11/L304 The effect of solidity, blade section, and contravane angle on the characteristics of an axial-flow fan / 1
Y 3.N 21/5:11/L305 The effects of angle of dead rise and angle of afterbody keel on the resistance of a model of a flying-boat hull / 1