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National Advisory Committee for Aeronautics Collection
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Pressure Distribution and Damping in Steady Pitch at Supersonic Mach Numbers of Flat Swept-Back Wings Having All Edges Subsonic
Sintering mechanism between zirconium carbide and columbium
Wind-Tunnel Investigation at Low Speed of the Lateral Control Characteristics of an Unswept Untapered Semi-Span Wing of Aspect Ratio 3.13 Equipped With Various 25-Percent-Chord Plain Ailerons
Measurement of the moments of inertia of an airplane by a simplified method
Effect of heat and power extraction on turbojet-engine performance 3: analytical determination of effects of shaft-power extraction
Boundary-layer measurements in 3.84- by 10-inch supersonic channel
Gust-tunnel investigation of a wing model with semichord line swept back 60 degrees
Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper: Mach lines behind flap leading and trailing edges
Analysis of shear strength of honeycomb cores for sandwich constructions
Free Oscillations of an Atmosphere in Which Temperature Increases Linearly With Height
Impact-Pressure Interpretation in a Rarefied Gas at Supersonic Speeds
An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds
Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7
Theory of helicopter damping in pitch or roll and a comparison with flight measurements
Theoretical investigation and application of transonic similarity law for two dimensional flow
Effect of Heat-Capacity Lag on a Variety of Turbine-Nozzle Flow Processes
The NACA Oil-Damped V-G Recorder
A flight investigation and analysis of the lateral-oscillation characteristics of an airplane
Effect of Heat-Capacity Lag on the Flow Through Oblique Shock Waves
The Effect of Ice Formations on Propeller Performance
Investigations of Slot Configurations for Film-Cooled Turbine Blades by Flow Visualization Methods
Low-Speed Aerodynamic Characteristics of a Series of Swept Wings Having NACA 65A006 Airfoil Sections (Revised)
Evaluation of a Ducted-Fan Power Plant Designed for High Output and Good Cruise Fuel Economy
Investigation of ignition characteristics of AN-F-32 and two AN-F-58a fuels in single can-type turbojet combustor
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