Browse TRAIL Inventories

Measurements of atmospheric turbulence over a wide range of wavelength for one meteorological condition

Measurements of boundary-layer transition at low speed on two bodies of revolution in a low-turbulence wind tunnel

Measurement of the longitudinal moment of inertia of a flexible airplane

Evaporation of JP-5 fuel sprays in air streams

Effects of two trailing-edge controls on the aerodynamic characteristics of a rectangular wing and body combination at Mach numbers from 3.00 and 5.05

Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28

A preliminary investigation of the static stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28

Exploratory investigation at a Mach number of 5.20 of the longitudinal aerodynamic characteristics of flat-bottom bodies

Further investigation of the feasibility of the freeze-casting method for forming full-size infiltrated titanium carbide turbine blades

Fuselage side inlets : a study of some factors affecting their performance and a comparison with nose inlets

Impingement of water droplets on a rectangular half body in a two-dimensional incompressible flow field

Friction studies of graphite and mixtures of graphite with several metallic oxides and salts at temperatures to 1000 F

Heat-transfer measurements on two bodies of revolution at a Mach number of 3.12

Heat-Requirements for Ice Protection of a Cyclically Gas-Heated, 36 Degree Swept Airfoil with Partial-Span Leading-Edge Slat

Heat-capacity measurements of titanium and of a hydride of titanium for temperatures from 4 to 15 K including a detailed description of a special adiabatic specific-heat calorimeter

Use of effective momentum thickness in describing turbine rotor-blade losses

On the permeability of porous materials

Full-scale wind-tunnel tests of the longitudinal stability and control characteristics of the XV-1 convertiplane in the autorotating flight range

Distribution of normal component of induced velocity in lateral plane of a lifting rotor

The effect of conical camber on the static longitudinal, lateral, and directional characteristics of a 45-degree sweptback wing at Mach numbers up to 0.96

Effect of concentration on ignition delays for various fuel-oxygen-nitrogen mixtures at elevated temperatures

Correlation of creep-buckling tests with theory

Drag coefficients for droplets and solid spheres in clouds accelerating in airstreams

Drag at model trim lift of a 1/15-scale Convair B-58 supersonic bomber

The use of perforated inlets for efficient supersonic diffusion

Design and test of mixed-flow impellers 7: experimental results for parabolic-bladed impeller with alternate blades cut back to form splitter vanes

Analytical investigation of factors affecting the performance of single-stage turbines having rotor-tip discharge of cooling air

Analytical investigation of single-stage-turbine efficiency characteristics in terms of work and speed requirements

Aerodynamic control of supersonic inlets for optimum performance

Calculated reactivity of uranyl-fluoride - water criticality experiments

Analytical determination of the natural coupled frequencies and mode shapes and the response to oscillating forcing functions of tandem helicopters

Transition-flight tests of a model of a low-wing transport vertical-take-off airplane with tilting wing and propellers

Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by a free-oscillation method

Aerodynamic design of axial-flow compressors Volume 1

Bending tests of ring-stiffened circular cylinders

A bibliography of NACA reports on control of turbojet engines

The Compressible Laminar Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient

Component performance investigation of J71 experimental turbine VI : effect of first-stator adjustment; over-all performance of J71-97 turbine with 70-percent-design stator area

Component performance investigation of J71 experimental turbine VIII : effect of first-stator adjustment; internal flow conditions of J71-97 turbine with 70-percent-design stator area

Analysis of elastic thermal stresses in thin plate with spanwise and chordwise variations of temperature and thickness

Analysis of laminar incompressible flow on semiporous channels

Analysis of a flight investigation at supersonic speeds of a simple homing system

Bodies of revolution having minimum drag at high supersonic airspeeds

The change with mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic speeds

Component performance of J71-A-2(600-D1) turbojet engine at several Reynolds number indices

Compressive stress-strain properties of 2024-T3 aluminum-alloy sheet at elevated temperatures

Compressive and torsional buckling of thin-wall cylinders in yield region

Compressive stress-strain properties of 7075-T6 aluminum-alloy sheet at elevated temperatures

Analysis of an automatic control to prevent rolling divergence

Boundary layer behind shock or thin expansion wave moving into stationary fluid


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