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- Section characteristics of an NACA 0006 airfoil with area suction near the leading edge
- Experimental stress analysis of stiffened cylinders with cutouts: Pure bending
- An experimental investigation of wheel spin-up drag loads
- The hydrodynamic characteristics of modified rectangular flat plates having aspect ratios of 1.00 and 0.25 and operating near a free water surface
- Hovering performance of a helicopter rotor using NACA 8-H-12 airfoil sections
- Dynamic stability and control characteristics of a cascade-wing vertically rising airplane model in take-offs, landings, and hovering flight
- Effects of panel flexibility on natural vibration frequencies of box beams
- An experimental study of porosity characteristics of perforated materials in normal and parallel flow
- Experimental stress analysis of stiffened cylinders with cutouts: Shear load
- Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates
- Transverse oscillations in a cylindrical combustion chamber
- Theoretical investigation of the effects upon lift of a gap between wing and body of a slender wing-body combination
- Transient temperature in heat exchangers for supersonic blowdown tunnels
- A theoretical investigation of the aerodynamics of wing-tail combinations performing time-dependent motions at supersonic speeds
- Turbulent boundary-layer and skin-friction measurements in axial flow along cylinders at Mach numbers between 0.5 and 3.6
- The zero-lift drag of a 60 degree delta-wing-body combination (AGARD model 2) obtained from free-flight tests between Mach numbers of 0.8 and 1.7
- A theoretical investigation of the heating-up period of injected fuel droplets vaporizing in air
- Time-temperature parameters and an application to rupture and creep of aluminum alloys
- Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal acceleration control system and a comparison with other types of systems
- Use of aerodynamic heating to provide thrust by vaporization of surface coolants
- Low speed yawed-rolling and some other elastic characteristics of two 56-inch-diameter, 24-ply-rating aircraft tires
- Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory
- Smoke study of nozzle secondary flows in a low-speed turbine
- Some aspects of the helicopter noise problem
- Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on the effectiveness of a plain flap at high subsonic Mach numbers
- Effect of heat treatment upon the microstructure and hardness of a wrought cobalt-base alloy stellite 21 (AMS 5385)
- A calculation study of wing-aileron flutter in two degrees of freedom for two-dimensional supersonic flow
- Fatigue tests at stresses producing failure in 2 to 10,000 cycles: 24S-T3 and 75S-T6 aluminum-alloy sheet specimens with a theoretical stress-concentration factor of 4.0 subjected to completely reversed axial load
- Analytical determination of the mechanism of an airplane spin recovery with different applied yawing moments by use of rotary-balance data
- Fatigue investigation of full-scale transport-airplane wings: Summary of constant-amplitude tests through 1953
- Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61
- Method for calculation of compressible laminar boundary layer with axial pressure gradient and heat transfer
- Study of three-dimensional internal flow distribution based on measurements in a 48-inch radial-inlet centrifugal impeller
- Some effects of aspect ratio and tail length on the contribution of a vertical tail to unsteady lateral damping and directional stability of a model oscillating continuously in yaw
- Some effects of exposure to exhaust-gas streams on emittance and thermoelectric power of bare-wire platinum rhodium - platinum thermocouples
- Torsional vibrations of hollow thin-walled cylindrical beams
- Approximate effect of leading-edge thickness, incidence angle, and inlet mach number on inlet losses for high-solidity cascades of low cambered blades
- An analytical and experimental study of the transient response of a pressure-regulating relief valve in a hydraulic circuit
- An analysis of the stability and ultimate bending strength of multiweb beams with formed-channel webs
- An experimental investigation at low speeds of the effects of lip shape on the drag and pressure recovery of a nose inlet in a body of revolution
- Generalized indicial forces on deforming rectangular wings in supersonic flight
- Experimental investigation at a Mach number of 2.41 of average skin-friction coefficients and velocity profiles for laminar and turbulent boundary layers and an assessment of probe effects
- Cooling requirements for stability of laminar boundary layer with small pressure gradient at supersonic speeds
- Density profiles of subsonic boundary layers on a flat plate determined by x-ray and pressure measurements
- Data on the compressive strength of skin-stringer panels of various materials
- Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees
- Wind-tunnel studies of the performance of multirotor configurations
- Calculated subsonic span loads and resulting stability derivatives of unswept and 45 degrees sweptback tail surfaces in sideslip and in steady roll
- Vaporization rates and drag coefficients for isooctane sprays in turbulent air streams
- A preliminary investigation of the effects of gusty air on helicopter-blade bending moments