๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Features of the Density Field of Dissociating Hypersonic Flows

โœ Scribed by H.G. Hornung


Publisher
John Wiley and Sons
Year
2000
Tongue
English
Weight
353 KB
Volume
80
Category
Article
ISSN
0044-2267

No coin nor oath required. For personal study only.

โœฆ Synopsis


Features of the Density Field of Dissociating Hypersonic Flows

The influence of dissociative chemical reactions on the flow fields encountered during flight into and out of the atmospheres of the inner planets is discussed. Blunt-body flow, and therefore the flow after a curved shock wave, is particularly relevant, and density is the variable that is most strongly affected, while it is at the same time the easiest to obtain field measurements of. The direction of the density gradient at the curved shock is determined analytically by obtaining a local solution of the Euler equation. The density gradient has two contributions: one from the shock curvature and one from the dissociation rate. Its direction undergoes a sudden change by 180 at a particular point on the shock, indicating a saddle point in the density field. The location of the saddle point is a sensitive indicator of the dissociation rate and directly provides an approximate measure of the reaction rate parameter. Experimental results are used to illustrate the theoretical findings. uey wordsX hyperveloity flowD dissoitive nonequiliriumD luntEody flowD urved shok wg (IWWIAX UTuHS


๐Ÿ“œ SIMILAR VOLUMES


Methods for the Accurate Computations of
โœ Kyu Hong Kim; Chongam Kim; Oh-Hyun Rho ๐Ÿ“‚ Article ๐Ÿ“… 2001 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 541 KB

In order to overcome some difficulties observed in the computation of hypersonic flows, a robust, accurate and efficient numerical scheme based on AUSM-type splitting is developed. Typical symptoms appearing in the application of AUSMtype schemes for high-speed flows, such as pressure wiggles near a

Methods for the Accurate Computations of
โœ Kyu Hong Kim; Chongam Kim; Oh-Hyun Rho ๐Ÿ“‚ Article ๐Ÿ“… 2001 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 938 KB

In order to eliminate or minimize the numerical error by shock waves due to grid distribution in multidimensional hypersonic flows, a new grid reconstruction scheme, the shock-aligned grid technique (SAGT), is proposed. The error due to shock waves in a non-shock-aligned grid system magnifies in pro