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Minimizing Aircraft ECS Bleed Off-Take - Virtual Integrated Aircraft Applications

Journal Article
2016-01-2054
ISSN: 1946-3855, e-ISSN: 1946-3901
Published September 20, 2016 by SAE International in United States
Minimizing Aircraft ECS Bleed Off-Take - Virtual Integrated Aircraft Applications
Sector:
Citation: Unlu, D., Cappuzzo, F., Broca, O., and Borrelli, P., "Minimizing Aircraft ECS Bleed Off-Take - Virtual Integrated Aircraft Applications," SAE Int. J. Aerosp. 9(1):151-162, 2016, https://doi.org/10.4271/2016-01-2054.
Language: English

References

  1. TOICA Thermal Overall Integrated Conception of Aircraft http://www.toica-fp7.eu May 2016
  2. Cappuzzo , F. , Broca , O. and Allain , L. Methodologies and Processes to Achieve Earlier Virtual Integration of Aircraft Systems presented at the 6th European Conference for Aerospace Sciences Krakow July 2015
  3. Pereira , G.C. , Turcio , W. H.L. , de Andrade , C. R. , Zaparoli , E.L. Heat transfer analysis of an aircraft cabin thermal transient Proceedings of the 10th Brazilian Congress of Thermal Sciences and Engineering 2004
  4. Ordonez , J.C , Bejan , A. 2001 Minimum power requirement for environmental control of aircraft Department of Mechanical Engineering and Material Science Duke University
  5. Conceição , S.T. , Zaparoli , E.L , Turcio , W.H.L Thermodynamic study of aircraft air conditioning air cycle machines: 3-wheel x 4-wheel 19th International Congress of Mechanical Engineering November 5-9, 2007 Brasilia, DF
  6. Ehlers , G.A. Selection of Turbomachinery - Centrifugal compressors Proceedings of the twenty-third turbomachinery symposium

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