Verification and validation studies of the time-averaged velocity field in the very near-wake of a finite elliptical cylinder

2004 ◽  
Vol 34 (4) ◽  
pp. 273-288 ◽  
Author(s):  
Michael R Flynn ◽  
Alfred D Eisner
2016 ◽  
Vol 97 (3) ◽  
pp. 715-728 ◽  
Author(s):  
Juan José Cruz Villanueva ◽  
Luís Fernando Figueira da Silva

Author(s):  
David Icove ◽  
Thomas May

Computer fire modeling can be a two-edged tool in forensic fire engineering investigations. Professional standards of care recommend that fire modeling’s primary use is in examining multiple hypotheses for a fire as opposed to determining its origin. This paper covers the current acceptable benefits of computer fire models, historical and pending legal case law, and methods to use modeling results within expert reports and testimony. Particular issues reviewed are the use of animations versus simulations, evidentiary guidelines, and authentication using verification and validation studies.


1972 ◽  
Vol 50 (16) ◽  
pp. 1842-1855 ◽  
Author(s):  
L. Sévigny ◽  
D. Heckman ◽  
A. Emond

The technique of measuring convection velocity in the hypersonic wake with a pair of in-line probes has been applied on a large scale to the mapping of the velocity field in the hypersonic wake through the use of a transverse survey array containing up to 8 ion-probe pairs. Measurements are reported of the velocity field in the wakes of 2.7 in. diameter spheres flown at 14 500 f/s in ballistic range atmospheres at 7.6 Torr and at 20 Torr of nitrogen. The array technique leads to convection velocity results which are in excellent agreement with the mean wake velocity data obtained by the sequential spark technique in an air atmosphere. In addition, the technique has permitted an extension of the mapping of the velocity field of 15 000 f/s spheres to considerably smaller axial distances than was possible with the spark method because of the difficulty of forming distinct sparks at the higher levels of ambient ionization encountered in the near wake.A comparison of the data obtained at 7.6 Torr and at 20 Torr shows that the amplitude of the velocity distribution in the wake, as defined by the velocity on the wake axis, is higher at higher pressure. Considering the wake width, however, it is found that the width of the velocity distribution is larger at the lower pressure of 7.6 Torr than is the case at 20 Torr, at least in the near wake. However, at axial distances greater than 300 or 400 diameters, the data for the two pressures tend to overlap. These observations appear to be related to other information indicating that for 2.7 in. diameter spheres launched at 7.6 Torr, the wake is not fully turbulent until about 300 or 400 diameters.


2005 ◽  
Author(s):  
K. Pickett ◽  
M. Flynn ◽  
Y. Koto ◽  
T. Anthony

1997 ◽  
Vol 4 (3) ◽  
pp. 125-136 ◽  
Author(s):  
J. Duan ◽  
S. Wiggins

Abstract. In this paper we study Lagrangian transport in the near wake of the flow around an obstacle, which we take to be a cylinder. In this case, for the range of Reynolds numbers investigated, the flow is two-dimensional and time periodic. We use ideas and methods from transport theory in dynamical systems to describe and quantify transport in the near wake. We numerically solve the Navier-Stokes equations for the velocity field and apply these methods to the resulting numerical representation of the velocity field. We show that the method of lobe dynamics can be used in conjunction with computational fluid dynamics methods to give very detailed and quantitative information about Lagrangian transport. In particular, we show how the stable and unstable manifolds of certain saddle-type stagnation points on the cylinder, and one in the wake, can be used to divide the flow into three distinct regions, an upper wake, a lower wake, and a wake cavity. The significance of the division using stable and unstable manifolds lies in the fact that these invariant manifolds form a template on which the transport occurs. Using this, we compute fluxes from the upper and lower wakes into the wake cavity using the associated turnstile lobes. We also compute escape time distributions as well as compare transport properties for two different Reynolds numbers.


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