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- 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
- 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
- Determination of stresses in gas-turbine disks subjected to plastic flow and creep
- Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners : panels that fail by local buckling and have various values of width-to-thickness ratio for the webs of the stiffeners
- Effect of yaw at supersonic speeds on theoretical aerodynamic coefficients of thin pointed wings with several types of trailing edge
- Effect of reducing valve overlap on engine and compound-power-plant performance