B. Fortunato, INVISCID AND VISCOUS-FLOW COMPUTATIONS BY MEANS OF A LAMBDA-METHODOLOGY - A REVIEW, Progress in aerospace sciences, 33(7-8), 1997, pp. 513-538
The present paper provides a review of the more important results obta
ined by the author, sometimes with co-authors, solving inviscid and vi
scous compressible flows by means of a lambda methodology. In particul
ar, an implicit numerical algorithm, called fast solver, has always be
en applied. This methodology separately integrates the compatibility c
onditions, written in terms of generalized Riemann variables, along ap
propriate bicharacteristic lines. The multi-dimensional flow problem i
s, thus, reduced to a sequence of simple quasi one-dimensional problem
s. The merits of this approach are demonstrated by means of the applic
ation of the method to the solution of three dimensional (3-D) subsoni
c and transonic inviscid flows, of two-dimensional (2-D) and 3-D visco
us flows and of the 2-D flow around a vertical axis wind turbine. In t
he transonic case the shock wave is computed by means of a shock fitti
ng technique, which enforces the proper shock jumps by an explicit use
of the Rankine-Hugoniot equations; in the wind turbine case the blade
s are represented in a time-averaged sense by means of an actuator por
ous cylinder, having the turbine radius. The results are then compared
with other numerical results and with experimental results. (C) 1997
Elsevier Science Ltd.