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- Effect of Reynolds number in turbulent-flow range on flame speeds of Bunsen-burner flames
- An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line designed to produce a high critical Mach number
- Evaluation of a fixed spoiler as a gust alleviator
- Effect of longitudinal stiffeners on the buckling load of long flat plates under shear
- The effects of variations in Reynolds number between 3.0 x 10 to the power 6 and 25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections
- Effects of temporal tangential bearing acceleration on performance characteristics of slider and journal bearings
- Effects of nacelle position on wing-nacelle interference
- Estimation of effectiveness of flap-type controls on sweptback wings
- Experimental investigation of the effects of plastic flow in a tension panel with a circular hole
- The effect of fuel composition, compression pressure, and fuel-air ratio on the compression-ignition characteristics of several fuels
- Tables of hypergeometric functions for use in compressible-flow theory
- A statistical analysis of gust-velocity measurements as affected by pilots and airplanes
- Supersonic wave drag of nonlifting sweptback tapered wings with Mach lines behind the line of maximum thickness
- A simplified method for the determination and analysis of the neutral-lateral-oscillatory-stability boundary
- Some fundamental similarities between boundary-layer flow at transonic and low speeds
- Sound from dual-rotating and multiple single-rotating propellers
- Sound-level measurements of a light airplane modified to reduce noise reaching the ground
- Properties of 19-9DL alloy bar stock at 1200 F
- Shear lag in axially loaded panels
- A study of skin temperatures of conical bodies in supersonic flight
- Effects of surface finish, of certain defects, and of repair of defects by welding on fatigue strength of 355-T6 sand-castings and effects of prior fatigue stressing on tensile properties
- Dynamometer-stand investigation of the muffler used in the demonstration of light-airplane noise reduction
- Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions
- A general small-deflection theory for flat sandwich plates
- An Investigation of Aircraft Heaters XXVIII : Equations for Steady-State Temperature Distribution Caused by Thermal Sources in Flat Plates Applied to Calculation of Thermocouple Errors, Heat-meter Corrections, and Heat Transfer by Pin-fin Plates
- Theoretical basic span loading characteristics of wings with arbitrary sweep, aspect ratio, and taper ratio
- Take-off performance of light twin-float sea- planes
- Theoretical evaluation of the ducted-fan turbojet engine
- A theoretical investigation of the effect of yawing moment due to rolling on lateral oscillatory stability
- Two-dimensional compressible flow in conical mixed-flow compressors
- Two-dimensional unsteady lift problems in supersonic flight
- Ultimate stresses developed by 24S-T and Alclad 75S-T aluminum-alloy sheet in incomplete diagonal tension
- The inward bulge type buckling of monocoque cylinders IV : experimental investigation of cylinders subjected to pure bending
- The inward bulge type buckling of monocoque cylinders V : revised strain energy theory which assumes a more general deflected shape at buckling
- Low-speed wind-tunnel investigation of various plain-spoiler configurations for lateral control on a 42 degree sweptback wing
- Methods of constructing charts for adjusting test results for the compressive strength of plates for differences in material properties
- Mollier diagrams for air saturated with water vapor at low temperatures
- Notes on the Lagrangian multiplier method in elastic-stability analysis
- The rupture-test characteristics of heat-resistant sheet alloys at 1700 F and 1800 F
- Quantitative analysis of ternary mixtures of naphthalene, 1-methylnaphthalene, and 2-methylnaphthalene by ultraviolet spectrophotometry
- Stability derivatives of triangular wings at supersonic speeds
- Stability derivatives of thin rectangular wings at supersonic speeds : wing diagonal ahead of tip mach lines
- An analysis of the airspeeds and normal accelerations of Sikorsky S-42A airplanes in commercial transport operation
- High-speed wind-tunnel investigation of an NACA 65-210 semispan wing equipped with plug and retractable ailerons and a full-span slotted flap
- The Development of Cambered Airfoil Sections Having Favorable Lift Characteristics at Supercritical Mach Numbers
- Development of cast aluminum alloys for elevated-temperature service
- An analysis of the airspeeds and normal accelerations of Martin M-130 airplanes in commercial transport operation
- Control considerations for optimum power proportionment in turbine-propeller engines
- Effect of taper ratio on low-speed static and yawing stability derivatives of 45 degree sweptback wings with aspect ratio of 2.61
- Influence of leading-edge suction on lift-drag ratios of wings at supersonic speeds