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