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Thermodynamic optimization of geometry in environmental control systems for aircraft

Publication ,  Journal Article
Bejan, A
Published in: International Journal of Heat and Technology
January 1, 2000

This review draws attention to an emerging body of work that relies on global thermodynamic optimization in the pursuit of flow system architecture. Exergy analysis establishes the theoretical performance limit. Thermodynamic optimization (or entropy generation minimization) brings the design as closely as permissible to the theoretical limit. The design is destined to remain imperfect because of constraints (finite sizes, times and costs). Improvements are registered by spreading the imperfection (e.g., flow resistances) through the system. Optimal spreading means spatial and temporal distribution, geometric form, rhythm, topology, and geography. System architecture springs out of constrained global optimization. The principle is illustrated by simple examples from the optimization of energy-system design for aircraft: The cruising speed for minimum exergy destruction, and the structure of heat exchangers for environmental control systems.

Duke Scholars

Published In

International Journal of Heat and Technology

ISSN

0392-8764

Publication Date

January 1, 2000

Volume

18

Issue

2

Start / End Page

3 / 10

Related Subject Headings

  • Mechanical Engineering & Transports
  • 51 Physical sciences
  • 02 Physical Sciences
 

Citation

APA
Chicago
ICMJE
MLA
NLM
Bejan, A. (2000). Thermodynamic optimization of geometry in environmental control systems for aircraft. International Journal of Heat and Technology, 18(2), 3–10.
Bejan, A. “Thermodynamic optimization of geometry in environmental control systems for aircraft.” International Journal of Heat and Technology 18, no. 2 (January 1, 2000): 3–10.
Bejan A. Thermodynamic optimization of geometry in environmental control systems for aircraft. International Journal of Heat and Technology. 2000 Jan 1;18(2):3–10.
Bejan, A. “Thermodynamic optimization of geometry in environmental control systems for aircraft.” International Journal of Heat and Technology, vol. 18, no. 2, Jan. 2000, pp. 3–10.
Bejan A. Thermodynamic optimization of geometry in environmental control systems for aircraft. International Journal of Heat and Technology. 2000 Jan 1;18(2):3–10.

Published In

International Journal of Heat and Technology

ISSN

0392-8764

Publication Date

January 1, 2000

Volume

18

Issue

2

Start / End Page

3 / 10

Related Subject Headings

  • Mechanical Engineering & Transports
  • 51 Physical sciences
  • 02 Physical Sciences