Thermal Optimization of Exhaust Assembly for Tractor Trailer

Author:

Mukutmoni Devadatta1,Gona Kiran2,Kandasamy Satheesh3,Li Han4,Rajagopal Anirudh4,Sugiyama Zen4

Affiliation:

1. Dassault Systemes: Dassault Systemes SE, Propulsion Group

2. Volvo Truck North America

3. Dassault Systeme North America

4. Dassault Systeme

Abstract

<div class="section abstract"><div class="htmlview paragraph">The horizontal exhaust in trucks is preferred over the vertical exhaust stack since the cost of production is lower than that of the vertical stack. The horizontal exhaust also comes with lower fuel costs since the overall drag coefficient is lower than that of the vertical stack. However, since a horizontal exhaust exits into the underbody, it is essential to minimize the exit temperatures of the exhaust to keep component temperatures within design limits.</div><div class="htmlview paragraph">In this study, a shape optimization is executed for the exhaust tip geometry to reduce exhaust exit temperatures while maintaining exhaust pressure by employing a computational fluid dynamics (CFD) workflow, using the geometry and morphing tool PowerDELTA®, coupled simulation approach between PowerFLOW® the flow solver and PowerTHERM® the thermal solver and Isight® for executing the optimization objectives.</div><div class="htmlview paragraph">A good correlation is observed with experimental data for the baseline truck design. The optimization process significantly reduced the exit temperatures of the exhaust. The optimal design performance was confirmed by installing the optimized exhaust geometry to the full vehicle, running the full-vehicle simulation, and observing a similar reduction in the exit temperature of the exhaust.</div></div>

Publisher

SAE International

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3. Ball , C.G. , Fellouah , H. , and Pollard , A. The Flow Field in Turbulent Round Free Jets Progress in Aerospace Sciences 50 2012 1 26

4. Kaushik , M. , Kumar , R. , and Humrutha , G. Review of Computational Fluid Dynamics Studies on Jets American Journal of Fluid Dynamics 5 3A 2015 1 11

5. De Young , D.S. Mass Entrainment in Astrophysical Jets Astrophysical Journal, Part 1 307 1986 62 72

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