TRAIL - Technical Report Archive and Image Library

Stability and control characteristics at low speed of an airplane model having a 38.7 degree sweptback wing with aspect ratio 4.51, taper ratio 0.54, and conventional tail surfaces

Flight determination of wing and tail loads on a fighter-type airplane by means of strain-gage measurements

Flight measurements of the longitudinal stability, stalling, and lift characteristics of an airplane having a 35 degrees sweptback wing without slots and with 40-percent-span slots and a comparison with wind-tunnel data

Flight measurements of the stability, control, and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-span slots and a comparison with wind-tunnel data

Bearing tests of 14S sheet and plate

Flow of a compressible fluid past a symmetrical airfoil in a wind tunnel and in free air

An Investigation of Aircraft Heaters 26: Development of a Sensitive Plated-Type Thermopile for Measuring Radiation

Investigation of a 1/7-scale powered model of a twin-boom airplane and a comparison of its stability, control, and performance with those of a similar all-wing airplane

Investigation of the validity of an ideal theory of elasto-plasticity for wrought aluminum alloys

Investigation of the variation of maximum lift for a pitching airplane model and comparison with flight results

A method of cycle analysis for aircraft gas-turbine power plants driving propellers

Flight measurements of the flying qualities of five light airplanes

Investigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing alone

Test of six types of Bakelite-bonded wire strain gages

Performance tests of wire strain gages 6: effect of temperature on calibration factor and gage resistance

Performance of conical jet nozzles in terms of flow and velocity coefficients

Performance of exhaust-gas blowdown turbine and various engine systems using a 12-cylinder liquid-cooled engine

Nonlinear large-deflection boundary-value problems of rectangular plates

The flexible rectangular wing in roll at supersonic flight speeds

Wind-tunnel investigation of effects of tail length on the longitudinal and lateral stability characteristics of a single-propeller airplane model

Lateral stability and control characteristics of a free-flying model having an unswept wing with an aspect ratio of 2

Load distributions due to steady roll and pitch for thin wings at supersonic speeds

Bearing strength of some aluminum-alloy sand castings

Bearing strengths of some aluminum-alloy rolled and extruded sections

Friction coefficients in the inlet length of smooth round tubes

Friction of solid films on steel at high sliding velocities

Friction at high sliding velocities of surfaces lubricated with sulfur as an additive

Heat transfer to bodies traveling at high speed in the upper atmosphere

Hydrodynamic impact loads in rough water for a prismatic float having an angle of dead rise of 30 degrees

Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds

Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness

Effect of exhaust pressure on knock-limited performance of an air-cooled aircraft-engine cylinder

Effect of chordwise location of maximum thickness on the supersonic wave drag of sweptback wings

Effect of compressibility on normal-force, pressure, and load characteristics of a tapered wing of NACA 66-series airfoil sections with split flaps

Critical axial-compressive stress of a curved rectangular panel with a central chordwise stiffener

Critical shear stress of an infinitely long plate in the plastic region

Divergence of swept wings

Downwash and wake behind untapered wings of various aspect ratios and angles of sweep

Determination of bending moments in pressure-loaded rings of arbitrary shape when deflections are considered

Design and Performance of Family of Diffusing Scrolls with Mixed-flow Impeller and Vaneless Diffuser

A linearized solution for time-dependent velocity potentials near three-dimensional wings at supersonic speeds

Theoretical distribution of lift on thin wings at supersonic speeds (An extension)

Apparent effect of inlet temperature on adiabatic efficiency of centrifugal compressors

Calculated performance of a compression-ignition engine-compressor-turbine combination based on experimental data

Calculated effects of geometric dihedral on the low-speed rolling derivatives of swept wings

Calculated performance of 12-cylinder liquid-cooled engine with exhaust-gas turbine geared to crankshaft

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