The current work deals with the methodology and results for the numerical modeling, research and implementation of an unconventional propulsion system for an airship with an innovative shape. It is a part of a global study (European Project MAAT) that investigates the possibilities of using the cruiser/feeders concept for passengers and cargo transportation. Based on an initial research for the airship shape, aerodynamic features at given altitudes, and the propulsion needs, were analyzed by means of numerical simulations for different flow conditions and propulsion concepts. The propulsion system is a set of air-jets, distributed in a circular row around the airship. The air-jets are working with an ambient air that is sucked/blowned from channels positioned in the upper and bottom sides of the airship body. These jets generate thrust to drive the airship in horizontal direction. The flow is modeled using the RANS equations with an appropriate model for turbulence effects simulation. The environmental conditions are varied in order to be representative of several altitude positions for the airship. Boundary zones that were set are “pressure far field”, “mass flow inlet”, “wall” and “fluid”. Attention is focused on the performance of the air-jets working with high mass flow rates and low jet flow speeds. They should also work in different combinations to ensure the needed thrust and direction of flight. The results provide opportunities for future developments of these propulsion concepts for airships.

Numerical Research on Efficiency Performance of the Propulsion System for an Innovative Airship / Ilieva, G; Pascoa, J; Dumas, Antonio; Trancossi, Michele. - STAMPA. - 6:(2012), pp. 573-579. (Intervento presentato al convegno ASME 2012 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2012 tenutosi a Chicago, IL, usa nel August 12–15, 2012) [10.1115/DETC2012-70927].

Numerical Research on Efficiency Performance of the Propulsion System for an Innovative Airship

DUMAS, Antonio;TRANCOSSI, MICHELE
2012

Abstract

The current work deals with the methodology and results for the numerical modeling, research and implementation of an unconventional propulsion system for an airship with an innovative shape. It is a part of a global study (European Project MAAT) that investigates the possibilities of using the cruiser/feeders concept for passengers and cargo transportation. Based on an initial research for the airship shape, aerodynamic features at given altitudes, and the propulsion needs, were analyzed by means of numerical simulations for different flow conditions and propulsion concepts. The propulsion system is a set of air-jets, distributed in a circular row around the airship. The air-jets are working with an ambient air that is sucked/blowned from channels positioned in the upper and bottom sides of the airship body. These jets generate thrust to drive the airship in horizontal direction. The flow is modeled using the RANS equations with an appropriate model for turbulence effects simulation. The environmental conditions are varied in order to be representative of several altitude positions for the airship. Boundary zones that were set are “pressure far field”, “mass flow inlet”, “wall” and “fluid”. Attention is focused on the performance of the air-jets working with high mass flow rates and low jet flow speeds. They should also work in different combinations to ensure the needed thrust and direction of flight. The results provide opportunities for future developments of these propulsion concepts for airships.
2012
ASME 2012 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2012
Chicago, IL, usa
August 12–15, 2012
6
573
579
Ilieva, G; Pascoa, J; Dumas, Antonio; Trancossi, Michele
Numerical Research on Efficiency Performance of the Propulsion System for an Innovative Airship / Ilieva, G; Pascoa, J; Dumas, Antonio; Trancossi, Michele. - STAMPA. - 6:(2012), pp. 573-579. (Intervento presentato al convegno ASME 2012 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2012 tenutosi a Chicago, IL, usa nel August 12–15, 2012) [10.1115/DETC2012-70927].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11380/981523
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