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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
https://izlik.org/JA83DF29EB

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
https://izlik.org/JA83DF29EB

Abstract

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Details

Primary Language English
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
IZ https://izlik.org/JA83DF29EB
Published in Issue Year 2006 Volume: 9 Issue: 4

Cite

APA Alabi, K., Ladeinde, F., Von Spakovsky, M., Moorhouse, D., & Camberos, J. (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. https://izlik.org/JA83DF29EB
AMA 1.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. https://izlik.org/JA83DF29EB
Chicago Alabi, Kehinde, Foluso Ladeinde, Michael Von Spakovsky, David Moorhouse, and Jose Camberos. 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. https://izlik.org/JA83DF29EB.
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 [1]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, Dec. 2006, [Online]. Available: https://izlik.org/JA83DF29EB
ISNAD Alabi, Kehinde - Ladeinde, Foluso - Von Spakovsky, Michael - Moorhouse, David - Camberos, Jose. “The Use of the 2nd Law As a Potential Design Tool for Aircraft Air Frame Subsystems”. International Journal of Thermodynamics 9/4 (December 1, 2006): 193-205. https://izlik.org/JA83DF29EB.
JAMA 1.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, Dec. 2006, pp. 193-05, https://izlik.org/JA83DF29EB.
Vancouver 1.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 [Internet]. 2006 Dec. 1;9(4):193-205. Available from: https://izlik.org/JA83DF29EB