scispace - formally typeset
ReportDOI

Regions and transitions of nonstationary oblique shock-wave diffractions in perfect and imperfect gases

G. Ben-Dor
- Vol. 79, pp 13307
TLDR
In this article, the authors investigated the diffraction of shock waves in perfect and imperfect nitrogen and argon by sharp compressive corners (2 deg or = Theta sub w or = 60 deg) and established the transition boundaries between these regions.
Abstract
: The diffraction of shock waves (2 or = M sub s or = 8) in perfect and imperfect nitrogen and argon by sharp compressive corners (2 deg or = Theta sub w or = 60 deg) were investigated analytically and experimentally. It is shown that seven shock-wave diffraction domains exist in nitrogen and six in argon in the ranges 1 or = M subs or = 10 and 0 deg or = Theta sub w or = 90 deg. The domains consist of the four well-known shock wave reflections, i.e., regular reflection (RR), single-Mach (SMR), complex-Mach (CMR) and double-Mach (DMR) reflections. All the transition boundaries between these regions were established analytically and substantiated by the present experimental results as well as the data from other sources. Over 100 experiments were conducted in the UTIAS 10 x 18 cm Hypervelocity Shock Tube equipped with a 23-cm dia field of view Mach-Zehnder interferometer equipped with a dual-frequency laser light source. It is shown that real-gas effects have a significant influence on the size of the regions and their transition boundaries. Some comparison between steady and nonstationary reflections are made and discussed. Isopycnics (lines of constant density) as well as density distributions along the wedge surface are presented for the various diffraction processes and their differences and similarities are discussed. (Author)

read more

Citations
More filters
Journal ArticleDOI

Regular and Mach Reflection of Shock Waves

TL;DR: In this article, a review of the literature in the field of shock reflection is presented, with explicit reference to the important authors omitted in the text unless their work is relatively recent.
Book

Front tracking and two dimensional Riemann problems

TL;DR: In this article, a numerical solution for the Mach reflection, a general classification scheme for two-dimensional elementary waves, and a discussion of problems and conjectures in this area are presented.
Journal ArticleDOI

Transonic dip mechanism of flutter of a sweptback wing. II

TL;DR: In this paper, an experimental investigation of the RR—-MR and MR-*RR transitions over concave and convex, smooth and rough wedges revealed that the wedge angle at which transition takes place (for a given Mach number) decreases and for a mesh 40 sand paper type surface roughness, the transition angle becomes independent of the incident shock wave Mach number.
Journal ArticleDOI

The phenomena of shock wave reflection — a review of unsolved problems and future research needs

TL;DR: The status of the research of the phenomenon of shock wave reflection is discussed in general, and unresolved problems and future research needs are pointed out as discussed by the authors, and a special scientific meeting dedicated to better understanding the reflection phenomena of shock waves, namely "The International Mach Reflection Symposium" was initiated in 1981 and was held since then in the major research centers actively involved in the research in shock wave reflections.
Journal ArticleDOI

A State-of-the-Knowledge Review on Pseudo-Steady Shock-Wave Reflections and their Transition Criteria

TL;DR: The double-Mach reflection (DMR) wave was first observed and reported by Smith (OSRD Rep. 6271, Off. Sci. Rep. Res. II-10, Princeton Univ. Dept.