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- Full-Scale Investigation of the Blade Motion of the PV-2 Helicopter Rotor
- Present status of research on boundary-layer control
- Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
- Preliminary investigation of a variable Mach number two-dimensional supersonic tunnel of fixed geometry
- Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds
- Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section.Transonic-bump method
- Investigation of the NACA-4-(3)(08)-03 two-blade propeller at forward Mach numbers to 0.925
- Investigation of the NACA 4-(4)(06)-04 two-blade propeller at forward Mach numbers to 0.925
- Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method
- Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section.Transonic-bump method
- Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60
- Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65-series wings equipped with full-span slotted flaps
- An Investigation of a Full-Scale Model of the Republic XF-91 Airplane in the Ames 40- By 80-Foot Wind Tunnel: Pressure Data
- Heat Transfer from High-Temperature Surfaces to Fluids III - Correlation of Heat-Transfer Data for Air Flowing in Silicon Carbide Tube with Rounded Entrance, Inside Diameter of 3/4 Inch, and Effective Length of 12 Inches
- Landing Procedure in Model Ditching Tests of Bf 109
- Systematic model researches on the stability limits of the DVL series of float designs
- Calibration Tests of a Japanese Log Rodmeter
- Calibration Tests of a German Log Rodmeter
- Investigation of Stability and Control Characteristics of a 1/10-scale Model of a Canadian Tailless Glider in the Langley Free-flight Tunnel
- Flight Test of the Aerojet 7KS-6000 T-27 Jato Rocket Motor
- Performance of Axial-Flow Supersonic Compressor of the XJ55-FF-1 Turbojet Engine. IV - Analysis of Compressor Operation over a Range of Equivalent Tip Speeds from 801 to 1614 Feet Per Second
- Performance of Axial-Flow Supersonic Compressor on XJ-55-FF-1 Turbojet Engine. I - Preliminary Performance of Compressor, 1, Preliminary Performance of Compressor
- Performance of Axial-Flow Supersonic Compressor of XJ55-FF-1 Turbojet Engine, III, Over-All Performance of Compressor
- Investigation of the Effect of Tip Tanks on the Wing Loading of a Republic F-84 Airplane in the Ames 40- by 80-foot Wind Tunnel
- Heat Transfer from High-Temperature Surfaces to Fluids. III - Correlation of Heat-Transfer Data for Air Flowing in Silicon Carbide Tube with Rounded Entrance, Inside Diameter of 3/4 Inch, and Effective Length of 12 Inches, Part 3, Correlation of Heat-Transfer Data for Air Flowing in Silicon Carbide Tube with Rounded Entrance, Inside Diameter of 3/4 Inch, and Effective Length of 12 Inches
- Effect of Air Cooling of Turbine Disk on Power and Efficiency of Turbine from Turbo Engineering Corporation TT13-18 Turbosupercharger.
- Investigation of flow coefficient of circular, square, and elliptical orifices at high pressure ratios
- Determination of rate, area, and distribution of impingement of of waterdrops on various airfoils from trajectories obtained on the differential analyzer
- A review of instruments developed for the measurement of the meteorological factors conductive to aircraft icing
- Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings
- Investigation of flow coefficient of circular, square, and elliptical orifices at high pressure ratios
- High-lift and lateral control characteristics of an NACA 652-215 semispan wing equipped with plug and retractable ailerons and a full-span slotted flap
- Influence of wing flexibility on force-time relation in shock strut following vertical landing impact
- Method for evaluating from shadow or Schlieren photographs the pressure drag in two-dimensional or axially symmetrical flow phenomena with detached shock
- The method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack
- Method of determining conditions of maximum efficiency of an independent turbine-propeller combination
- Oxidation characteristics of molybdenum disulfide and effect of such oxidation on its role as a solid-film lubricant
- Laminar mixing of a compressible fluid
- Longitudinal flying qualities of several single-rotor helicopters in forward flight
- Further experiments on the flow and heat transfer in a heated turbulent air jet
- On the flying qualities of helicopters
- Determination of plate compressive strengths at elevated temperatures
- Effect of forebody warp and increase in afterbody length on the hydrodynamic qualities of a flying-boat hull of high length-beam ratio
- Corrosion tests of a heated wing utilizing an exhaust-gas-air mixture for ice prevention
- Critical shear stress of infinitely long, simply supported plate with transverse stiffeners
- Critical axial-compressive stress of a curved rectangular panel with a central longitudinal stiffener
- Critical shear stress of a curved rectangular panel with a central stiffener
- Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow
- Determination of centrifugal-compressor performance on basis of static-pressure measurements in vaneless diffuser
- Biaxial fatigue strength of 24S-T aluminum alloy