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The Use of the 2nd Law as a Potential Design Tool for Aircraft Air Frame Subsystems

Year 2006, Volume: 9 Issue: 4, 193 - 205, 01.12.2006

Abstract

This paper presents the modeling of the irreversible thermodynamics of the Air Frame Subsystem as a component of integrated aircraft design/synthesis. Entropy calculation procedures for complicated geometries in curvilinear coordinates are described, including the effects of turbulence. Both inviscid and viscous calculations are reported and the contributions of the various terms in the entropy equation are investigated. The procedure is validated and then extended to the calculation of entropy generation associated with flow over the B747200 aircraft. Results show that most of the entropy generation is due to turbulence. The viscous dissipation term in the entropy equation dominates compared to the heat transfer term. The implications of the results for design improvement are briefly discussed.

Year 2006, Volume: 9 Issue: 4, 193 - 205, 01.12.2006

Abstract

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Details

Primary Language English
Journal Section Regular Original Research Article
Authors

Kehinde Alabi This is me

Foluso Ladeinde This is me

Michael Von Spakovsky

David Moorhouse This is me

Jose Camberos This is me

Publication Date December 1, 2006
Published in Issue Year 2006 Volume: 9 Issue: 4

Cite

APA Alabi, K., Ladeinde, F., Von Spakovsky, M., Moorhouse, D., et al. (2006). The Use of the 2nd Law as a Potential Design Tool for Aircraft Air Frame Subsystems. International Journal of Thermodynamics, 9(4), 193-205.
AMA Alabi K, Ladeinde F, Von Spakovsky M, Moorhouse D, Camberos J. The Use of the 2nd Law as a Potential Design Tool for Aircraft Air Frame Subsystems. International Journal of Thermodynamics. December 2006;9(4):193-205.
Chicago Alabi, Kehinde, Foluso Ladeinde, Michael Von Spakovsky, David Moorhouse, and Jose Camberos. “The Use of the 2nd Law As a Potential Design Tool for Aircraft Air Frame Subsystems”. International Journal of Thermodynamics 9, no. 4 (December 2006): 193-205.
EndNote Alabi K, Ladeinde F, Von Spakovsky M, Moorhouse D, Camberos J (December 1, 2006) The Use of the 2nd Law as a Potential Design Tool for Aircraft Air Frame Subsystems. International Journal of Thermodynamics 9 4 193–205.
IEEE K. Alabi, F. Ladeinde, M. Von Spakovsky, D. Moorhouse, and J. Camberos, “The Use of the 2nd Law as a Potential Design Tool for Aircraft Air Frame Subsystems”, International Journal of Thermodynamics, vol. 9, no. 4, pp. 193–205, 2006.
ISNAD Alabi, Kehinde et al. “The Use of the 2nd Law As a Potential Design Tool for Aircraft Air Frame Subsystems”. International Journal of Thermodynamics 9/4 (December 2006), 193-205.
JAMA Alabi K, Ladeinde F, Von Spakovsky M, Moorhouse D, Camberos J. The Use of the 2nd Law as a Potential Design Tool for Aircraft Air Frame Subsystems. International Journal of Thermodynamics. 2006;9:193–205.
MLA Alabi, Kehinde et al. “The Use of the 2nd Law As a Potential Design Tool for Aircraft Air Frame Subsystems”. International Journal of Thermodynamics, vol. 9, no. 4, 2006, pp. 193-05.
Vancouver Alabi K, Ladeinde F, Von Spakovsky M, Moorhouse D, Camberos J. The Use of the 2nd Law as a Potential Design Tool for Aircraft Air Frame Subsystems. International Journal of Thermodynamics. 2006;9(4):193-205.