Browse TRAIL Inventories

Fatigue-crack-propagation and residual-static-strength results on full-scale transport-airplane wings

Tests with hydrogen fuel in a simulated afterburner

An experimental study of the zero-angle-of attack transonic drag associated with the vertical position of a horizontal tail at zero incidence

Some experiments relating to the problem of simulation of hot jet engines in studies of jet effects on adjacent surfaces at a free-stream Mach number of 1.80

A theoretical analysis of heat transfer in regions of separated flow

The effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems

Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at Mach numbers from 0 to 1.9

Effect of camber on the drag of a body of revolution

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

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


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