Investigation to define the propagation characteristics of a finite amplitude acoustic pressure wave Final report
Aerodynamic noise generation by finite amplitude pressure wave propagation through entropy producing regions
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Aerodynamic noise generation by finite amplitude pressure wave propagation through entropy producing regions
Outwardly propagating coronal Alfven waves pressure exertion on solar wind, using one fluid polytrope model
A series of experiments was conducted to investigate temporal and spatial velocity distributions of fluid flow in 3-in. open-end pipes of various lengths up to 210 ft, produced by the propagation of nonlinear pressure waves of various intensities. Velocity profiles across each of five sections along the pipes were measured as a function of time with the use of hot-film and hot-wire anemometers for two pressure waves produced by a piston. Peculiar configurations of the velocity profiles across the pipe section were noted, which are uncommon for steady pipe flow. Theoretical consideration was given to this phenomenon of higher velocity near the pipe wall for qualitative confirmation. Experimentally time-dependent velocity distributions along the pipe axis were compared with one-dimensional theoretical results obtained by the method of characteristics with or without diffusion term for the purpose of determining the attenuation characteristics of the nonlinear wave propagation in the pipes.
Periodic shock fronted longitudinal pressure wave effect on instantaneous heat flux rates at tube end wall
Shock wave pressure decay in polycarbonate targets impacted by hypervelocity cylindrical projectile
Harmonic content of pressure wave shapes in strong traveling transverse acoustic modes
Apparatus for generating HF shock fronted pressure waves in resonant tube
One dimensional models of pressure wave propagation through annular and mist flows
A theoretical analysis of the propagation characteristics of a finite amplitude pressure wave is presented. The analysis attempts to study the contribution of entropy-producing regions to the mechanism of aerodynamic noise generation. It results in a nonlinear convective wave equation in terms of entropy and a thermodynamic 'J' function. A direct analogy between the derived governing equation and those used in classical literature is obtained. An idealization of the processes considered permits the uncoupling of the equations of motion with a consequent construction of an acoustic analogy treating shock wave emission of finite amplitude acoustic waves. An engineering approach is reflected in the concept of an extended plug nozzle whose function is to facilitate aerodynamic noise attenuation by modifying the entropy-producing regions.
Ground measurements of shock wave pressure for fighter aircraft at very low altitudes
In-flight shock wave pressure measurements above and below bomber aircraft at mach 1.42 to 1.69
The specific area of an aqueous foam contained in a tube is obtained by determining the fraction of the quantity of light emitted by a source and diffused by the specific area of the column of the foam. The velocity of the waves of weak pressure (which propagate in the air with the velocity of sound) is measured by noticing the moment when the wave penetrates the column and the moment when, having reached the opposite side, it determines a variation of the light diffused by the area of the latter.
Mechanical behavior of anesthetized dog abdominal vena cava from pressure wave transmission characteristics, discussing chemical and electrical stimuli
Temporal and spatial flow velocity profiles produced by shock tube generated pressure wave propagation in open-end pipe
A numerical study of finite-strength, isentropic pressure waves transverse to the axis of a circular cylinder was made for the radial resonant mode. The waves occur in a gas otherwise at rest, filling the cylinder. A method of characteristics was used for the numerical solution. For small but finite amplitudes, calculations indicate the existence of waves of permanent potential form. For larger amplitudes, a shock is indicated to occur. The critical value of the initial amplitude parameter in the power series is found to be 0.06 to 0.08, under various types of initial conditions.
Ground measurements of shock-wave pressure for two supersonic low-flying fighter aircraft
Effect of periodic shock-fronted pressure waves on instantaneous heat flux at end wall of shock tube
Elastic behavior of large blood vessels in canine aorta by measuring dispersion and attenuation of artificially induced pressure waves