INCAS TRISONIC WIND TUNNEL

The 1.2 m x 1.2 m Trisonic Blowdown Wind Tunnel is the largest of the experimental facilities at the National Institute for Aerospace Research - I.N.C.A.S. "Elie Carafoli", Bucharest, Romania. The tunnel has been designe...

Low-Order GAM Admire System in Landing Preparation Phase

In this paper the symbolic and numeric computations for the simplified GAM (Generic Aerodynamic Model) Admire system are presented . The numeric computations were performed into the MatLab environment with the aim of pre...

Determination of flow front velocity and optimal injection pressures for better impregnation of E-glass with polyester in resin transfer mold

Flow front velocity of resin plays a key role in yielding better impregnation of fiber reinforcement in resin transfer molding to fabricate quality composites. A video camera was used to capture the patterns of resin flo...

Two phase flow models in DxUNSp code platform

The aim of this work is to find an efficient implementation for a two phase flow model in an existing URANS CFD code platform (DxUNSp), initially based on unsteady URANS equations with a k-ε turbulence model and various...

BOOK REVIEWS: Problems of Quantitative Methods. Algebra, Trigonometry, Analytical Geometry and Mathematical Analysis (Part I) - Probleme de metode cantitative. Algebra, trigonometrie, geometrie analitica si analiza matematica (Partea I), Sorin BERBENTE, Corneliu BERBENTE Published by Editura Universitatii Romano-Britanice, Seria “Business”, Bucuresti, 2006, ISBN (10) 973-87669-1-5/ ISBN (13) 978-