Browse TRAIL Inventories

Flying qualities of a high-performance personal-owner airplane

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) : body of revolution with near-parabolic forebody and cylindrical afterbody

Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities

Experimental investigation of an 0.8 hub-tip radius-ratio,nontwisted-rotor-blade turbine

Preliminary investigation of the pressure fluctuations in the wakes of two-dimensional wings at low angles of attack

Jet effects on pressures and drags of bodies

Preliminary investigation of use of conical flow separation for efficient supersonic diffusion

Applicability of the hypersonic similarity rule to pressure distributions which include the effects of rotation for bodies of revolution at zero angle of attack

Experimental investigation of a 16-inch impulse-type supersonic-compressor rotor

Effects of Reynolds number on the aerodynamic characteristics of a delta wing at Mach number of 2.41

Experimental investigation of air-cooled turbine blades in turbojet engine 9: evaluation of the durability of noncritical rotor blades in engine operation

Experimental investigation of air-cooled turbine blade in turbojet engine 8: rotor blades with capped leading edges

Effects of double-slotted flaps and leading-edge modifications on the low-speed characteristics of a large-scale 45 degrees swept-back wing with and without camber and twist

Data presentation of force characteristics of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0 / Robert T. Madden and Emil J. Kremzier

Effects of altitude on turbojet engine performance

Base pressures measured on several parabolic-arc bodies of revolution in free flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers

Basic pressure measurements on a fuselage and a 45 degrees sweptback wing-fuselage combination at transonic speeds in the slotted test section of the Langley 8-foot high-speed tunnel

Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98

Wind-tunnel tests of a 1/12-scale model of the X-3 airplane at subsonic and supersonic speeds.

Comparison of drag, pressure recovery, and surface pressure of a scoop-type inlet and an NACA submerged inlet at transonic speeds

A specially constructed metallograph for use at elevated temperatures

Relation of engine turbine-blade life to stress-rupture properties of the alloys, Stellite 21, Hastelloy B, Cast S-816, Forged S-816, X-40, Nimonic 80, Refractory 26, N-155, and Iconel X

A recurrence matrix solution for the dynamic response of aircraft in gusts

Investigation of the liquid fluorine-liquid diborane propellant combination in a 100-pound-thrust rocket engine

Buckling of thin-walled cylinder under axial compression and internal pressure

Variation of the pressure limits of flame propagation with tube diameter for propane-air mixtures

Vaporization rates and heat-transfer coefficients for pure liquid drops

Experimental investigation of typical constant- and variable-area exhaust nozzles and effects on axial-flow turbojet-engine performance

The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil

An investigation of the control-surface flutter derivatives of an NACA 65(sub 1)-213 airfoil in the Ames 16-foot high-speed wind tunnel

Direct-reading design charts for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded Z-section stiffeners

Experimental investigation of turbojet-engine thrust augmentation by combined compressor coolant injection and tail-pipe burning

Flame velocities over a wide composition range for pentane-air, ethylene-air, and propyne-air flames

The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight

Full-scale investigation of cooling shroud and ejector nozzle for a turbojet engine: afterburner installation

Free-spinning tunnel investigation of the 1/21-scale model of the Chance Vought F7U-3 airplane: TED No. NACA DE 362

Optical methods involving light scattering for measuring size and concentration of condensation particles in supercooled hypersonic flow

Correlation of analog solutions with experimental sea-level transient data for controlled turbine-propeller engine, including analog results at altitudes

Analytical investigation of flow through high-speed mixed-flow turbine

Aerodynamic characteristics of a slender cone-cylinder body of revolution at a Mach number of 3.85

Characteristics of a transonic test section with various slot shapes in the Langley 8-foot high-speed tunnel

Compressive strength of flanges

An analysis of base pressure at supersonic velocities and comparison with experiment

Evaluation of the reduced-mass method of representing wing-lift effects in free-fall drop tests of landing gears

System analyses and autopilot design for automatic roll stabilization of a supersonic pilotless aircraft

A simplified instrument for recording and indicating frequency and intensity of icing conditions encountered in flight

A study of effects of viscosity on flow over slender inclined bodies of revolution

A small-deflection theory for curved sandwich plates

The static longitudinal characteristics at Mach numbers up to 0.95 of a triangular-wing canard model having a triangular control

Summary of Methods for Calculating Dynamic Lateral Stability and Response and for Estimating Lateral Stability Derivatives


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