Details
We wish to thank the following for their contribution to the success of this conference: ONRG, Office of Naval Research Global, United States. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author(s) and do not necessarily reflect the views of the Office of Naval Research Global."
Aircraft have evolved into extremely complex machines, posing a highly integrated design challenge, including many energy interrelated systems dependent. Some of the systems also generate by-products, in the form of heat that must be carefully addressed. Methods exist for the design of all these systems, based on the evolutionary vehicle development. However, the more we depart from existing databases and experience levels, the less confident we are in an optimal design. In addition, many of the classical techniques remain constrained by the simplifying assumptions used in their original derivation. If these are not considered, then there is no guide to when those classical techniques no longer give an energy-optimum solution.
The objective of these lecture series proceedings is to present a common design currency in the form of “exergy,” as the potential work available from an energy source. It is the thesis of this work to explain and develop the theory of explicit exergy-based design, with validating design examples. The course will start with a general lecture covering the background of 2nd Law of Thermodynamics analysis. Then the basics of the method are presented followed by applications of the fundamental theory. The course note continues with discussions of subsonic vehicle, gas turbine and combustion applications. Finally, hypersonic analysis is presented followed by discussions on the integrated system approach and design space visualization methods.
Together, the application of exergy methods to all levels of flight vehicle design is presented. The notes provide a good basis for engineers working in all areas of vehicle design.
- MOORHOUSE, D. & CAMBEROS, J. – Air Force Research Laboratory, USA
Systems Fundamentals - CAMBEROS, J.1 & DOTY, J.2 - 1Air Force Research Laboratory & 2The University of Dayton, USA
Exergy Analysis: Theoretical Foundations - DOTY, J. – Air Force Research Laboratory / The University of Dayton, USA
System Applications - BOWCUTT, K. – The Boeing Company, USA
Hypersonic Systems MDAO - FIGLIOLA, R. – Clemson University, USA
Applications of exergy analysis to subsonic aerodynamic systems design - ROTH, B. – General Electric, USA
Propulsion system analysis - VILLACE, V.F. & PANIAGUA, G. – von Karman Institute for Fluid Dynamics, Belgium
Modeling and second principle analysis of combined-cycle engines for high speed propulsion - GRÖNSTEDT, T. – Chalmers University of Technology, Sweden
Propulsion Systems Modeling - RIGGINS, D. – Missouri University of Science and Technology, USA
High-speed aero-propulsion integration - BEJAN, A. – Duke University, USA
Entropy generation minimization and the constructal law - VAN SPAKOVSKY, M. – Virginia Tech, USA
Mission integrated analyses and optimizations - LAMBE, L. – Multidisciplinary Software Systems Research Corporation, USA
Mathematical foundations for physics-based simulations - GERMAN, B.J. & DASKILEWICZ, M.J. – Georgia Institute of Technology, USA
Multivariate data visualization for engineering design
Additional Information
| Manufacturer | von Karman Institute for Fluid Dynamics |
|---|
Check items to add to the cart or select all
You have no items in your shopping cart.
