Browse TRAIL Inventories

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

Comparison of computed performance of composite power plants using 18-cylinder aircraft engines with 62 degrees and 40 degrees valve overlap

Analysis of performance of a jet engine from characteristics of components II : interaction of components as determined from engine operation

Bending of rectangular plates with large deflections

Characteristics of thin triangular wings with triangular-tip control surfaces at supersonic speeds with Mach lines behind the leading edge

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

Compressible flow tables for air

Compressive buckling of simply supported plates with transverse stiffeners

Biaxial plastic stress-strain relations for 24S-T aluminum alloy

The effect of variations in moments of inertia on spin and recovery characteristics of a single- engine low-wing monoplane with various tail arrangements, including a twin tail

Effect of pressure recovery on the performance of a jet-propelled airplane

Determination of transient skin temperature of conical bodies during short-time, high-speed flight


Published Year

Subject

Author

‹‹ previous 1 2 ... 111 112 113 114 115 116 117 ... 280 281 next ››