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- Results of axial-load fatigue tests on electropolished 2024-T3 and 7075-T6 aluminum-alloy-sheet specimens with central holes
- Properties of aircraft fuels
- Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9
- Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes
- Theoretical study of the lateral frequency response to gusts of a fighter airplane, both with controls fixed and with several types of autopilots
- A theoretical study of the aerodynamics of slender cruciform-wing arrangements and their wakes
- Low-speed yawed-rolling characteristics and other elastic properties of a pair of 26-inch-diameter, 12-ply-rating, type VII aircraft tires
- Minimum wave drag for arbitrary arrangements of wings and bodies
- Calculations of the rate of thermal dissociation of air behind normal shock waves at Mach numbers of 10, 12, and 14
- Investigation of the effect of short fixed diffusers on starting blowdown jets in the Mach number range from 2.7 to 4.5
- A method for calculating the contour of bodies of revolution with a prescribed pressure gradient at supersonic speed with experimental verification
- A preliminary investigation of the effects of frequency and amplitude on the rolling derivatives of an unswept-wing model oscillating in roll
- A method for deflection analysis of thin low-aspect-ratio wings
- Investigation of the effects of ground proximity and propeller position on the effectiveness of a wing with large-chord slotted flaps in redirecting propeller slipstreams downward for vertical take-off
- Some effects of fuselage flexibility on longitudinal stability and control
- Analysis of the ultimate strength and optimum proportions of multiweb wing structures
- Approximate indicial lift functions for several wings of finite span in incompressible flow as obtained from oscillatory lift coefficients
- Investigation of the propulsive characteristics of a helicopter-type pulse-jet engine over a range of Mach numbers and angle of yaw
- Effect of climb technique on jet-transport noise
- Wind-tunnel investigation of effects of fuselage cross-sectional shape, fuselage bend, and vertical-tail size on directional characteristics of nonoverlap-type helicopter fuselage models without rotors
- On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders
- Experimental investigation of the flow around lifting symmetrical double-wedge airfoils at Mach numbers of 1.30 and 1.41
- Investigation of the compressive strength and creep lifetime of 2024-T aluminum-alloy skin-stringer panels at elevated temperatures
- Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
- Investigation of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy plates at elevated temperatures
- Theoretical analysis of linked leading-edge and trailing-edge flap-type controls at supersonic speeds
- Gust-load and airspeed data from one type of two-engine airplane on six civil airline routes from 1947 to 1955
- An experimental investigation of the scale relations for the impinging water spray generated by a planing surface
- Experimental investigation of the vibrations of a built-up rectangular box beam
- Particular solutions for flows at Mach number 1
- Flow studies on drooped-leading-edge delta wings at supersonic speed
- Effect of shallow water on the hydrodynamic characteristics of a flat-bottom planing surface
- A Transonic Wind-Tunnel Investigation of a Seaplane Configuration having a 40 Deg Sweptback Wing, TED No. NACA DE 387
- Aerodynamic design of axial-flow compressors: Volume 3
- Friction, wear, and surface damage of metals as affected by solid surface films
- Intensity, scale, and spectra of turbulence in mixing region of free subsonic jet
- Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees
- Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition
- The near noise field of static jets and some model studies of devices for noise reduction
- Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data
- A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition
- On the Kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow
- Effect of chord size on weight and cooling characteristics of air-cooled turbine blades
- Static Longitudinal and Lateral Stability and Control Data Obtained from Tests of a 1/15-Scale Model of the Goodyear XZP5K Airship, TED No. NACA DE 211
- Hovering-flight tests of a model of a transport vertical-take-off airplane with tilting wing and propellers
- Component performance investigation of J71 experimental turbine I : over-all performance with 97-percent-design stator areas
- The proper combination of lift loadings for least drag on a supersonic wing
- Effect of Wing Height and Dihedral on the Lateral Stability Characteristics at Low Lift of a 45 Deg Swept-Wing Airplane Configuration as Obtained from Time-Vector Analyses of Rocket-Propelled-Model Flights at Mach Numbers from 0.7 to 1.3
- Propagation of a free flame in a turbulent gas stream
- Some possibilities of using gas mixtures other than air in aerodynamic research