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NACA Technical Notes
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Reciprocity relations in aerodynamics
Investigation of Statistical Nature of Fatigue Properties
A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachines of Axial-, Radial-, and Mixed-Flow Types
Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed
The effects of Reynolds number on the application of NACA 16-series airfoil characteristics to propeller design
Orientation of orifices on bodies of revolution for determination of stream static pressure at supersonic speeds
Design of two-dimensional channels with prescribed velocity distribution along the channel walls 1: relaxation solutions
An Impulse-Momentum Method for Calculating Landing-Gear Contact Conditions in Eccentric Landings
Investigation of Laminar Boundary Layer in Compressible Fluids Using the Crocco Method
Coincidence Method Applied to Ion Beam Measurement
Numerical determination of indicial lift and moment functions for a two-dimensional sinking and pitching airfoil at Mach numbers 0.5 and 0.6
Langley full-scale-tunnel investigations of the maximum-lift and stalling characteristics of a trapezoidal wing of aspect ratio 4 with circular-arc airfoil sections
Some dynamic effects of fuel motion in simplified model tip tanks on suddenly excited bending oscillations
flow studies in the vicinity of a modified flat-plate rectangular wing of aspect ratio 0.25
Bonding of molybdenum disulfide to various materials to form a solid lubricating film 1: the bonding mechanism
Experimental investigation of the local and average skin friction in the laminar boundary layer on a flat plate at a Mach number of 2.4
Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections
Correlation of Tensile Strength, Tensile Ductility, and Notch Tensile Strength With the Strength of Rotating Disks of Several Designs in the Range of Low and Intermediate Ductility
Analytical and Experimental Investigation of Fully Developed Turbulent Flow of Air in a Smooth Tube With Heat Transfer With Variable Fluid Properties
Compressive buckling of simply supported curved plates and cylinders of sandwich construction
Survey of the Chromium-Cobalt-Nickel Phase Diagram at 1200 C
Some Remarks on an Approximate Method of Estimating the Wave Drag Due to Thickness at Supersonic Speeds of Three-Dimensional Wings With Arbitrary Profile
Method for calculation of heat transfer in laminar region of air flow around cylinders of arbitrary cross section (including large temperature differences and transpiration cooling)
Survey of Portions of the Cobalt-Chromium-Iron-Nickel Quaternary System
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