Browse TRAIL Inventories

A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock

Experimental investigation of a 90 degree cascade diffusing bend with an area ratio of 1.45:1 and with several inlet boundary layers

Orientation of orifices on bodies of revolution for determination of stream static pressure at supersonic speeds

Comparison of supersonic minimum-drag airfoils determined by linear and nonlinear theory

Comparison of two- and three-dimensional potential-flow solutions in a rotating impeller passage

Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6

Effects of wing sweep on the upwash at the propeller planes of multiengine airplanes

Effects of wing lift and weight on landing-gear loads

Effects of solvents in improving boundary lubrication of steel by silicones

Application of linear analysis to an experimental investigation of a turbojet engine with proportional speed control

On the calculation of flow about objects traveling at high supersonic speeds

Stress and strain at onset of crazing of polymethyl methacrylate at various temperatures

Wear and sliding friction properties of nickel alloys suited for cages of high-temperature rolling-contact bearings I : alloys retaining mechanical properties to 600 F

Condensation of air in supersonic wind tunnels and its effects on flow about models

Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges

A vector study of linearized supersonic flow applications to nonplanar problems

Investigation with an interferometer of the flow around a circular-arc airfoil at mach numbers between 0.6 and 0.9

Laminar boundary layer on cone in supersonic flow at large angle of attack

A probability analysis of the meteorological factors conducive to aircraft icing in the United States

Gust-response analysis of an airplane including wing bending flexibility

Displacement effect of a three-dimensional boundary layer

Some experiments on visualization of flow fields behind low-aspect-ratio wings by means of a tuft grid

Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds

Experimental investigation of transition of a model helicopter rotor from hovering to vertical autorotation

Effects of Mach number variation between 0.07 and 0.34 and Reynolds number variation between 0.97 x 10(exp 6) and 8.10 x 10(exp 6) power on the maximum lift coefficient of a wing of NACA 64-210 airfoil sections

A comparison of the spanwise loading calculated by various methods with experimental loadings obtained on a 45 degrees sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)

Summary of stall-warning devices

flow studies in the vicinity of a modified flat-plate rectangular wing of aspect ratio 0.25

Measurements of temperature variations in the atmosphere near the tropopause with reference to airspeed calibration by the temperature method

A compressible-flow plotting device and its application to cascade flows

Boundary-layer development and skin friction at mach number 3.05

Altitude Investigation of Gas Temperature Distribution at Turbine of Three Similar Axial-Flow Turbojet Engines

Summary of Low-Lift Drag and Directional Stability Data from Rocket Models of the Douglas XF4D-1 Airplane with and without External Stores and Rocket Packets at Mach Numbers from 0.8 to 1.38: TED No. NACA DE-349

Altitude Starting Tests of a 1000-Pound-Thrust Solid-Propellant Rocket

Investigation of wear and friction properties under sliding conditions of some materials suitable for cages of rolling-contact bearings

Theoretical Investigation of the Effects of the Artificial-Feel System on the Maneuvering Characteristics of the F-89 Airplane

Analytical study of shimmy of airplane wheels

Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow

Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow

Preliminary air-flow and thrust calibrations of several conical Cooling-air ejectors with a primary to secondary temperature ratio of 1.0 I :diameter ratios of 1.21 and 1.10

Solubility of water in hydrocarbons

Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane IV : rectangular cowl inlets with two-dimensional compression ramps

Performance and operational characteristics of a python turbine-propeller engine at simulated altitude conditions / Carl L. Meyer and Lavern A. Johnson

Performance characteristics of canard-type missile with vertically mounted nacelle engines at Mach numbers 1.5 to 2.0

Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane 3: normal wedge inlet with semicircular cowl

Performance characteristics of canard-type missile with wing-mounted nacelle engines at Mach numbers 1.5 to 2.0

Recent data on controls

Some control considerations for ram-jet engines

Preliminary investigation of control characteristics at transonic speeds of a tapered 45 degree sweptback wing of aspect ratio 3 having a horn-balanced full-span control

Preliminary investigation of flow fluctuations during surge and blade row stall in axial-flow compressors / c Merle C. Huppert


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