By Gabi Ben-Dor
ISBN-10: 3540713816
ISBN-13: 9783540713814
This publication offers a accomplished state-of-the-knowledge description of the surprise wave mirrored image phenomena from a phenomenological element of view.
The first half is an intensive advent to indirect surprise wave reflections, proposing the 2 significant recognized mirrored image wave configurations, specifically, average (RR) and Mach (MR) reflections, the corresponding - and three-shock theories, their analytical and graphical resolution and the proposed transition obstacles among those reflection-wave configurations.
The moment, 3rd and fourth components describe the mirrored image phenomena in regular, pseudo-steady and unsteady flows, respectively. right here, the prospective particular forms of mirrored image wave configurations are defined, standards for his or her formation and termination are awarded and their governing equations are solved analytically and graphically and in comparison with experimental results.
The answer of the well known von Neumann paradox and a close description of 2 new reflection-wave configurations - the Guderely mirrored image (GR) and Vasilev mirrored image (VR) - also are given.
The 5th half is an in depth directory of the main suitable medical papers and study experiences which have been released to date within the box of concern wave mirrored image phenomena.
Intended as either advent and reference, this publication will gain scientists and engineers in surprise wave comparable educational and commercial learn and improvement, in addition to graduate scholars wishing to concentrate on the field.
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Additional resources for Shock Wave Reflection Phenomena (Springer 2007)
Sample text
Numerical simulation of weak shock diffraction over a wedge under the von Neumann paradox conditions”, Comp. Math. & Math. , 39, 1335–1345, 1999. , Dept. , Tech. Rep. , 1951. 2 Shock Wave Reflections in Steady Flows List of symbols Latin Letters Speed of sound in state (i) ai a Average speed of sound behind a curved Mach stem d Maximum horizontal shift of the foot of the Mach stem with respect to the triple point H Distances from the leading edge to the line of symmetry/bottom surface Distances from the triple point to the line of Hm symmetry/bottom (=length of the Mach stem for a straight Mach stem) Hm Nondimensional Mach stem height The height of the throat (see Fig.
Consequently, state 22 1 General Introduction Fig. 15. pi /p0 , θiR -polar solution of a regular reflection (2), which is obtained from state (1) by passing through the reflected shock wave, is on the R-polar. , the line along which θR = 0. 15 implies that two different points, (2w ) and (2s ), fulfill the just-mentioned requirement. 13)]. ” Note that none of these two solutions could be discarded on theoretical grounds. However, it is an experimental fact that, unless special measures are taken, the weak-shock solution is the one that usually occurs.
22a, b where two different (I–R)-polars combinations are shown. While in Fig. 22a, the R-polar intersects the p-axis along its “weak” portion in Fig. 22b the R-polar intersects the p-axis along its “strong” portion. Thus, while the flow behind the reflected shock wave is supersonic for the former case, it is subsonic for the latter. 5 Suggested RR IR Transition Criteria Pi P0 Pi P0 6 m s 6 m (2) 4 (2) 2 θi 10Њ I R (1) 0 s I R 2 1 31 1 20Њ (1) θi 0 10Њ (a) 20Њ (b) Pi P0 m (2) s 6 R 3 (1) I θi (0) 1 0 10Њ 20Њ (c) Fig.
Shock Wave Reflection Phenomena (Springer 2007) by Gabi Ben-Dor
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