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- Wind-tunnel investigation and analysis of the effects of end plates on the aerodynamic characteristics of an unswept wing
- Method of determining initial tangents of contours of flow variables behind a curved, axially symmetric shock wave
- Investigation of the air-compression process during drop tests of an oleo-pneumatic landing gear
- Vibratory stresses in propellers operating in the flow field of a wing-nacelle-fuselage combination
- Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel
- Charts for estimation of longitudinal-stability derivatives for a helicopter rotor in forward flight
- Theoretical aerodynamic characteristics of a family of slender wing-tail-body combinations
- Theoretical aerodynamic characteristics of bodies in a free-molecule-flow field
- A theoretical analysis of the effects of several auxiliary damping devices on the lateral stability and controllability of a high-speed aircraft
- Kinetics of sintering chromium carbide
- A biharmonic relaxation method for calculating thermal stress in cooled irregular cylinders
- A rapid approximate method for determining velocity distribution on impeller blades of centrifugal compressors
- The similarity law for hypersonic flow about slender three-dimensional shapes
- Wind-Tunnel Investigation of a Number of Total Pressure Tubes at High Angles of Attack
- Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack: Subsonic speeds
- Investigation at Mach number 1.91 of side and base pressure distributions over conical boattails without and with jet flow issuing from base
- Flight Camera for Photographing Cloud Droplets in Natural Suspension in the Atmosphere
- Flight measurements of the wing-dropping tendency of a straight-wing jet airplane at high subsonic Mach numbers
- Flight determined buffet boundaries of ten airplanes and comparisons with five buffeting criteria
- Investigation of internal film cooling of 1000-pound-thrust liquid-ammonia - liquid-oxygen rocket-engine combustion chamber
- Investigation of mechanisms of blade failure of forged Hastelloy B and cast Stellite 21 turbine blades in turbojet engine
- Investigation of torsion creep-to-rupture properties of N-155 alloy
- Investigation of off-design performance of shock-in-rotor type supersonic blading
- An investigation of single-degree-of-freedom snaking oscillations on a model of a high-speed research airplane by the NACA wing-flow method
- Preliminary investigation of effectiveness of base bleed in reducing drag of blunt-base bodies in supersonic stream
- Drag interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02
- Turbine performance characteristics of a python turbine-propeller engine investigated in altitude wind tunnel
- The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions
- Over-all performance of J35-A-23 two-stage turbine
- Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail: longitudinal characteristics
- Preliminary data on the effect of body-nose bluntness on the drag and pressure recovery of a side-inlet-body combination at Mach numbers of 1.4 and 1.7
- Preliminary evaluation of the air and fuel specific-impulse characteristics of several potential ram-jet fuels II : magnesium and magnesium - octene-1 slurries
- Preliminary study of circulation in an apparatus suitable for determining corrosive effects of hot flowing liquids
- Preliminary investigation of a submerged inlet and a nose inlet in the transonic flight range with free-fall models
- Preliminary evaluation of the air and fuel specific-impulse characteristics of several potential ram-jet fuels I : octene-1, aluminum, and aluminum - octene-1 slurries
- Preliminary investigation of a fin-actuated jet-vane control system for stabilization of rocket-powered models
- The preparation, physical properties, and heats of combustion of four alkylsilanes
- Large-Scale Flight Measurements of Zero-Lift Drag at Mach Numbers from 0.90 to 1.95 of an Arrow Wing in Combination with a Small Body
- Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span equal to 1
- Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span equal to and less than 1 and some static
- Large-scale flight measurements of zero-lift drag at Mach numbers from 0.8 to 1.6 of a wing-body combination having an unswept 4.5 percent thick wing with modified hexagonal sections
- Load-Range Performance of Turbine-Propeller Engine in Transonic Speed Range and Comparison with Load-Range Performance of Turbojet Engine
- Lift and drag coefficients for the Bell X-1 airplane (8-percent-thick wing) in power-off transonic flight
- Longitudinal frequency-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements, including a method for the evaluation of transfer functions
- Longitudinal-control effectiveness and downwash characteristics at a Mach number of 1.24 of a 1/30-scale semispan model of the Bell X-5 airplane as determined by the NACA wing-flow method
- Low-speed characteristics of a wing having 63 degrees sweepback and uniform camber
- Low-speed investigation of a 0.16 scale model of the X-3 airplane : lateral and directional characteristics
- Measurements of downwash and sidewash behind cruciform triangular wings at Mach number 1.4
- Measurement of distortion in second experimental control rod with temperature patterns simulating shim rod out and shim rod 50 percent inserted for Argonne Naval Reactor / A. F. Lietzke and T. F. Nagey
- Flame velocities of four alkylsilanes