Browse TRAIL Inventories

Effect of Length-Beam Ratio on the Aerodynamic Characteristics of Flying-Boat Hulls without Wing Interference

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

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

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

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.

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

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Investigation of a large-scale model at low speed

Experimental and Theoretical Studies of Area Suction for the Control of the Laminar Boundary Layer on a Porous Bronze NACA 64A010 Airfoil

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


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