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Implications of engine deterioration for fuel usage

Author

Listed:
  • Naeem, M.
  • Singh, R.
  • Probert, D.

Abstract

For an assumed aircraft's mission profile (consisting of several flight stages), using a bespoke computer simulation, the consequences of engine deterioration upon the weight of the fuel that has to be carried and consumed are predicted. This will help in making wiser management decisions (such as whether to remove an aero-engine from the aircraft for maintenance or to continue using it with some changes in the aircraft's mission profile). Hence, improved engine-utilisation can be achieved, so resulting in lower overall life-cycle costs.

Suggested Citation

  • Naeem, M. & Singh, R. & Probert, D., 1998. "Implications of engine deterioration for fuel usage," Applied Energy, Elsevier, vol. 59(2-3), pages 125-146, February.
    • Handle: RePEc:eee:appene:v:59:y:1998:i:2-3:p:125-146
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    Cited by:

    1. Zhang, Jiyuan & Tang, Hailong & Chen, Min, 2019. "Linear substitute model-based uncertainty analysis of complicated non-linear energy system performance (case study of an adaptive cycle engine)," Applied Energy, Elsevier, vol. 249(C), pages 87-108.
    2. Naeem, M. & Singh, R. & Probert, D., 1998. "Implications of engine deterioration for operational effectiveness of a military aircraft," Applied Energy, Elsevier, vol. 60(3), pages 115-152, July.
    3. Naeem, M. & Singh, R. & Probert, D., 1998. "Implications of engine deterioration for creep life," Applied Energy, Elsevier, vol. 60(4), pages 183-223, August.
    4. Naeem, M. & Singh, R. & Probert, D., 2001. "Consequences of aero-engine deteriorations for military aircraft," Applied Energy, Elsevier, vol. 70(2), pages 103-133, October.

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