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The Calculation of Span Load Distributions of Swept-Back Wings
Compressive Strength of 24S-T Aluminum-Alloy Flat Panels With Longitudinal Formed Hat-Section Stiffeners
An analysis of the airspeeds and normal accelerations of Boeing B-247 and B-247D airplanes in commercial transport operation
Recommendations for numerical solution of reinforced-panel and fuselage-ring problems
Notes and Tables for Use in the Analysis of Supersonic Flow
Determination of Ram-Jet Combustion-Chamber Temperatures by Means of Total-Pressure Surveys
Ceramic Coatings for Prevention of Carbon Absorption in Four Heat-Resistant Alloys
Effect of changing manifold pressure, exhaust pressure, and valve timing on the air capacity and output of a four-stroke engine operated with inlet valves of various diameters and lifts
Relation Between Inflammables and Ignition Sources in Aircraft Environments
Critical Combinations of Bending, Shear, and Transverse Compressive Stresses for Buckling of Infinitely Long Flat Plates
An investigation at subsonic speeds of several modifications to the leading-edge region of the NACA 64A010 airfoil section designed to increase maximum lift
Mechanical and Corrosion Tests of Spot-Welded Aluminum Alloys
Wind-tunnel investigation of jet-augmented flaps on a rectangular wing to high momentum coefficients
Method for Calculating Effects of Dissociation on Flow Variables in the Relaxation Zone Behind Normal Shock Waves
A Survey of Background and Aircraft Noise in Communities Near Airports
Experimental determination of the range of applicability of the transonic area rule for wings of triangular plan form
Wind-tunnel investigation at low speeds to determine the effect of aspect ratio and end plates on a rectangular wing with jet flaps deflected 85 degrees
Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence
Laminar Boundary Layer With Heat Transfer on a Cone at Angle of Attack in a Supersonic Stream
One-Dimensional, Compressible, Viscous Flow Relations Applicable to Flow in a Ducted Helicopter Blade
A Fundamental Investigation of Fretting Corrosion
Operating Characteristics of an Acceleration Restrictor as Determined by Means of a Simulator
Analytical determination of the mechanism of an airplane spin recovery with different applied yawing moments by use of rotary-balance data
Approximate effect of leading-edge thickness, incidence angle, and inlet mach number on inlet losses for high-solidity cascades of low cambered blades
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