Investigation of the spectral characteristics of gases heated by shock waves
Spectral characteristics of nitrogen, argon, air, and carbon dioxide and nitrogen mixtures at high temperatures and pressures
Ambartsumyan, Ye. N.↗
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Calculation of the onset time of equilibrium dissociation on the basis of experimental data concerning the nonstationary propagation of a reflected shock wave
Dissociation relaxation times of carbon dioxide
Bazhenova, T. V.↗
Study of shock waves in a nonequilibrium plasma.
Electron number density and temperature profiles in seeded Ar plasma supersonic flow past perpendicular flat disk
Christiansen, W. H.↗
Vibrations and dissociation coupling behind strong shock waves
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Marrone, P. V.↗
Shock wave shear layer interaction in clustered rocket exhausts Final report, 24 Jun. 1966 - 15 Oct. 1967
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Damkevala, R. J.↗
Unique intermetallic compounds prepared by shock wave synthesis
Technique compresses fine ground metallic powder mixture beyond crystal fusion point. Absence of vapor pressure voids and elimination of incongruous effects permit application of technique to large scale fabrication of intermetallic compounds with specific characteristics, e.g., semiconduction, superconduction, or magnetic properties.
Otto, G.↗
Experimental study of the shock wave due to a blunt leading edge in the hypersonic merged- flow regime
Measuring low-density flow over two-dimensional blunt bodies in hypersonic arc tunnel
Winebarger, R. M.↗
Perturbations behind thickened shock waves
Approximative sound wave scattering behind sonic boom overpressure signatures
Plotkin, K. J.↗
Nonlinear analysis of flow pulses and shock waves in arteries. I
Large amplitude wave propagation in arteries, deriving aorta mathematical model consistent with heart pressure and flow pulses and wavefront velocity
Anliker, M.↗
The effect of the bow shock wave on the stability of blunt nosed slender bodies
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Seiff, A.↗
Theoretical structure and spectrum of a shock wave in the interstellar medium - The Cygnus Loop.
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Cox, D. P.↗
Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock waves.
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Coe, C. F.↗
Analysis of sonic boom measurements near shock wave extremities for flight near Mach 1.0 and for airplane accelerations
The analysis of the 14 low-altitude transonic flights showed that the prevailing meteorological consideration of the acoustic disturbances below the cutoff altitude during threshold Mach number flight has shown that a theoretical safe altitude appears to be valid over a wide range of meteorological conditions and provides a reasonable estimate of the airplane ground speed reduction to avoid sonic boom noise during threshold Mach number flight. Recent theoretical results for the acoustic pressure waves below the threshold Mach number caustic showed excellent agreement with observations near the caustic, but the predicted overpressure levels were significantly lower than those observed far from the caustic. The analysis of caustics produced by inadvertent low-magnitude accelerations during flight at Mach numbers slightly greater than the threshold Mach number showed that folds and associated caustics were produced by slight changes in the airplane ground speed. These caustic intensities ranged from 1 to 3 time the nominal steady, level flight intensity.
Haglund, G. T.↗
A study of shock-wave turbulent boundary layer interaction using laser velocimeter and hot-wire anemometer techniques
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Rose, W. C.↗
Numerical solution of the interaction of a strong shock wave with a hypersonic turbulent boundary layer
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Baldwin, B. S.↗
Reynolds-shear-stress measurements in a compressible boundary layer within a shock-wave-induced adverse pressure gradient
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Rose, W. C.↗
A model for the propagation of flare-associated interplanetary shock waves
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Chao, J. K.↗
Interaction of strong shock wave with turbulent boundary layer
The reported investigation represents an extension of the time-dependent solution of separated laminar flows based on the complete Navier-Stokes equations reported by MacCormack (1971) and Carter (1973). The current study includes turbulence models in conjunction with the compressible flow equations. The calculations start with a uniform flow except for values imposed along the upstream and outer boundaries. The basic numerical method is discussed along with questions concerning the exponential accuracy and the resolution of the viscous sublayer in a compressed region.
Baldwin, B. S.↗