Lorris Charrier, Mathieu Jubera, Grégoire Pont, Simon Marié, Pierre Brenner and Francesco Grasso
The design of a space launcher requires some considerations about the unsteady loads and heat transfer occurring at the base of the structure. In particular, these phenomena are…
Abstract
Purpose
The design of a space launcher requires some considerations about the unsteady loads and heat transfer occurring at the base of the structure. In particular, these phenomena are predominant during the early stage of the flight. This paper aims to evaluate the ability of the unstructured, high order finite-volume CFD solver FLUSEPA, developed by Airbus Safran Launchers, to accurately describe these phenomena.
Design/methodology/approach
This paper first performs a steady simulation on a base flow around a four-clustered rocket configuration. Results are compared with NASA experiments and Loci-CHEM simulations. Then, unsteady simulations of supersonic H2/air reacting mixing layer based on the experiment of Miller, Bowman and Mungal are performed. Three meshes with different cells number are used to study the impact of spatial resolution. Instantaneous and time-averaged concentrations are compared with the combined OH/acetone planar laser-induced fluorescence imaging from the experiment.
Findings
FLUSEPA satisfactorily predicts the base heat flux at the base of a four-clustered rocket configuration. NASA Loci-CHEM reactive simulations indicate that afterburning plays an important role and should not be neglected. The unsteady reactive computation of a supersonic mixing layer shows that FLUSEPA is also able to accurately predict flow structures and interactions. However, the complexity of the experiment and the lack of details concerning the facility prevents from obtaining satisfactory converged results.
Originality/value
This study is the first step on the development of a cost-effective method aiming at predicting unsteady loads and heat transfer on space launchers using an unsteady and reactive model for the CDF calculations. It uses original techniques such as conservative CHIMERA-like overset grids, local re-centering of fluxes and local adaptive time-stepping to reduce computational cost while being robust and accurate.
Details
Keywords
Peter J. Baldacchino, Elena Marie’ Gatt and Simon Grima
In this chapter the authors identified and discussed the most significant barriers faced by cooperative movements in Malta, providing recommendations for potential solutions…
Abstract
In this chapter the authors identified and discussed the most significant barriers faced by cooperative movements in Malta, providing recommendations for potential solutions. Primary data for this research were collected through the use of semi-structured interviews with a selection of 18 representatives of the small current Maltese cooperative movement, most of whom are active either in individual cooperatives (16) and/or in the cooperative institutions (five).
Findings indicated that the most significant problems are the lack of education and awareness regarding the cooperative movement. These are closely followed by the divide within the movement itself, which is also hindering further development of Maltese cooperatives. Therefore, for the movement to grow and develop, one must first tackle the lack of education and awareness of this business model. Furthermore, in order for the movement to reach its full potential there must be cooperation amongst cooperatives, leading to the appropriate environment for growth.
Through the identification of these significant barriers, targeted action may be recommended and taken so as to reduce, if not eliminate, these barriers and thereby help the Maltese cooperative movement flourish.