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- Downwash characteristics and vortex-sheet shape behind a 63 degree swept-back wing-fuselage combination at a Reynolds number of 6.1 x 10(exp 6)
- Determination of viscosity of exhaust-gas mixtures at elevated temperatures
- Flight measurements of drag and base pressure of a fin-stabilized parabolic body of revolution (NACA RM-10) at different Reynolds numbers and at Mach numbers from 0.9 to 3.3
- Determination of flame temperatures from 2000 to 3000 K by microwave absorption
- Design considerations for wings having minimum drag due to lift
- Design data for multipost-stiffened wings in bending
- An analytical estimation of the effect of transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, turbulent boundary layer
- An analytical investigation of airplane spin-recovery motion by use of rotary-balance aerodynamic data
- Comparison of model and full-scale spin recoveries obtained by use of rockets
- Comparison of flutter calculations using various aerodynamic coefficients with experimental results for some rectangular cantilever wings at Mach number 1.3
- Combined natural- and forced-convection laminar flow and heat transfer of fluids with and without heat sources in channels with linearly varying wall temperatures
- Effect of various arrangements of triangular ledges on the performance of a 23 degree conical diffuser at subsonic Mach numbers
- Evaluation of the accuracy of an aircraft radio altimeter for use in a method of airspeed calibration
- Examination of the existing data on the heat transfer of turbulent boundary layers at supersonic speeds from the point of view of Reynolds analogy
- An evaluation of the soap-bubble method for burning velocity measurements using ethylene-oxygen-nitrogen and methane-oxygen-nitrogen mixtures
- Tables for the computation of wave drag of arrow wings of arbitrary airfoil section
- An evaluation of an accelerometer method for obtaining landing-gear drag loads
- Minimum-wave-drag airfoil section for arrow wings
- Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections
- The effectiveness at high subsonic Mach numbers of a 20-percent-chord plain trailing-edge flap on the NACA 65-210 airfoil section
- An experimental and theoretical investigation of the anisotropy of 3S aluminum-alloy sheet in the plastic range
- Experimental determination of boundary-layer transition on a body of revolution at M = 3.5
- Experimental investigation of heat-transfer and fluid-friction characteristics of white fuming nitric acid
- Experimental investigation of temperature recovery factors on a 10 degree cone at angle of attack at a Mach number of 3.12
- Impingement of Water Droplets on an Ellipsoid with Fineness Ration 10 in Axisymmetric Flow
- A simple mechanical analogue for studying the dynamic stability of aircraft having nonlinear moment characteristics
- Shock-turbulence interaction and the generation of noise
- Shocks in helical flows through annular cascades of stator blades
- Some new drag data on the NACA RM-10 missile and a correlation of the existing drag measurements at M = 1.6 and 3.0
- Some measurements and power spectra of runway roughness
- Some measurements of atmosphere turbulence obtained from flow-direction vanes mounted on an airplane
- A simplified mathematical model for calculating aerodynamic loading and downwash for wing-fuselage combinations with wings of arbitrary plan form
- Static properties and resistance characteristics of a family of seaplane hulls having varying length-beam ratio
- Relation of microstructure to high-temperature properties of a wrought cobalt-base alloy stellite 21 (AMS 5385)
- The resistance to air flow of porous materials suitable for boundary-layer-control applications using area suction
- 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