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Flight Studies of the Horizontal-Tail Loads Experienced by a Fighter Airplane in Abrupt Maneuvers
A general representation for axial-flow fans and turbines
Wind-tunnel investigation of control-surface characteristics 6: a 30-percent-chord plain flap on the NACA 0015 airfoil
Wind-tunnel investigation of control-surface characteristics 1: effect of gap on the aerodynamic characteristics of an NACA 0009 airfoil with a 30-percent-chord plain flap
Wind-Tunnel Investigation of a Plain and a Slot-Lip Aileron on a Wing With a Full-Span Flap Consisting of an Inboard Fowler and an Outboard Slotted Flap
Tire friction coefficients and their relation to ground-run distance in landing
An investigation of aircraft heaters 16: determination of the viscosity of exhaust gases from a gasoline engine
Wind-Tunnel Investigation of Control-Surface Characteristics 22: Medium and Large Aerodynamic Balances of Two Nose Shapes and a Plain Overhang Used With a 0.20-Airfoil-Chord Flap on an NACA 0009 Airfoil
Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane
Wind-Tunnel Investigation of Control-Surface Characteristics 14: NACA 0009 Airfoil With a 20-Percent-Chord Double Plain Flap
Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane 1: Measurements of Flying Qualities With Original Tail Surfaces
Experimental Determination of the Yawing Moment Due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model
The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-Flight Tunnel
A correlation of loadings and afterbody length-beam ratios of various flying-boat hulls
Wind-tunnel vibration tests of a four-blade single rotating pusher propeller
Recommended Test Procedure for Aircraft Engine Turbosupercharger Power Plants
Effect of various carburetor throttle settings on the flow characteristics at the outlet of a supercharger inlet elbow
Evaluation of the Induced-Velocity Field of an Idealized Helicopter Rotor
A Comparison of the Effects of Four-Blade Dual- and Single-Rotation Propellers on the Stability and Control Characteristics of a High-Powered Single-Engine Airplane
Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel
Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics 5: Symmetrically Tapered Wing With a Circular Fuselage Having a Horizontal and a Vertical Tail
An analytical study of wing and tail loads associated with an elevator deflection
Theoretical Investigation of Methods for Computing Drag From Wake Surveys at High Subsonic Speeds
The effect of dead rise upon the high-angle porpoising characteristics of two planing surfaces in tandem
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