Open Access
Issue
MATEC Web Conf.
Volume 304, 2019
9th EASN International Conference on “Innovation in Aviation & Space”
Article Number 02016
Number of page(s) 8
Section Flight Physics: Noise & Aerodynamics
DOI https://doi.org/10.1051/matecconf/201930402016
Published online 17 December 2019
  1. F. Majić, G. Efraimsson, and C. J. O'Reilly, “Potential improvement of aerodynamic performance by morphing the nacelle inlet,” Aerospace Science and Technology, vol. 54, pp. 122–131, 2016. [CrossRef] [Google Scholar]
  2. S. Kazula, M. Wöllner, D. Grasselt, and K. Höschler, “Ideal Geometries and Potential Benefit of Variable Pitot Inlets for Subsonic and Supersonic Business Aviation,” Proceedings of the 8th Eucass, 2019. [Google Scholar]
  3. L. da Rocha–Schmidt, A. Hermanutz, and H. Baier, “Progress Towards Adaptive Aircraft Engine Nacelles,” Proc. of the 29th Congress of the International Council of the Aeronautical Sciences, 2014. [Google Scholar]
  4. N. G. Ozdemir et al., “Morphing nacelle inlet lip with pneumatic actuators and a flexible nano composite sandwich panel,” Smart Mater. Struct., vol. 24, no. 12, p. 125018, 2015. [CrossRef] [Google Scholar]
  5. SAE Aerospace, ARP4754A. SAE International, 2010. [Google Scholar]
  6. S. Kazula, M. Wöllner, D. Grasselt, and K. Höschler, “Parametric design and aero–dynamic analysis of circular variable aero engine inlets for transonic and supersonic civil aviation,” Proc. of ISABE, 2019. [Google Scholar]
  7. S. Kazula and K. Höschler, “A systems engineering approach to variable intakes for civil aviation,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 095441001983690, 2019. [Google Scholar]
  8. S. Kazula, D. Grasselt, M. Mischke, and K. Höschler, “Preliminary safety assessment of circular variable nacelle inlet concepts for aero engines in civil aviation,” in Proceedings of the 28th ESREL, CRC Press, 2018, pp. 2459–2467. [Google Scholar]
  9. S. Kazula, D. Grasselt, and K. Höschler, “Common Cause Analysis of Circular Variable Nacelle Inlet Concepts for Aero Engines in Civil Aviation,” in Proceedings of the 6th International Conference on Integrity–Reliability–Failure :, 2018. [Google Scholar]
  10. S. Kazula and K. Höschler, “Ice detection and protection systems for circular variable nacelle inlet concepts,” CEAS Aeronaut J (2019). DOI 10.1007/s13272-019-00413-1. [Google Scholar]
  11. J. D. Mattingly, Elements of Propulsion: Gas Turbines and Rocket, AIAA, 2006. [Google Scholar]
  12. J. Seddon and E. L. Goldsmith, Intake aerodynamics, AIAA, 1999. [Google Scholar]
  13. W. J. G. Bräunling, Flugzeugtriebwerke, Springer Vieweg, 2015. [Google Scholar]
  14. S. Farokhi, Aircraft propulsion. Wiley, 2014. [Google Scholar]
  15. R. Hedayati and M. Sadighi, Bird strike. Woodhead Publishing, 2016. [Google Scholar]
  16. Rolls–Royce plc., The jet engine. Wiley, 2015. [Google Scholar]
  17. G. Akhras, “Nano & Smart NDE Systems – Applications in Aerospace and Perspectives,” 4th International Symposium on NDT in Aerospace, 2012. [Google Scholar]
  18. S. Murugan and M. I. Friswell, “Morphing wing flexible skins with curvilinear fiber composites,” Composite Structures, vol. 99, pp. 69–75, 2013. [CrossRef] [Google Scholar]
  19. M. Kintscher and M. Wiedemann, “Investigation of Multi–material Laminates for Smart Droop Nose Devices,” ICAS, 2014. [Google Scholar]
  20. M. Mischke, S. Kazula, and K. Höschler, “A Comparative Concept Study and Evaluation for New Broadband Noise Absorbing Acoustic Liner Concepts for Civil Aviation,” Proceedings of Global Power and Propulsion Society, 2019. [Google Scholar]
  21. Virginia Tech Intellectual Properties Inc., “Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors,” US5355417A. [Google Scholar]
  22. H. Schlichting, K. Gersten, and E. Krause, Grenzschicht–Theorie, Springer, 2006. [Google Scholar]
  23. H. G. Lueders, Experimental Investigation of Advanced Concepts to Increase Turbine Blade Loading. Washington, D.C.: NASA Lewis Research Center, 1968. [Google Scholar]
  24. A. L. Braslow, A History of Suction–Type Laminar–Flow Control with Emphasis on Flight Research. Monograph in Aerospace History, No. 13, 1999. NASA, 1999. [Google Scholar]
  25. J. Feldhusen and K.–H. Grote, Pahl/Beitz Konstruktionslehre, Springer Vieweg, 2013. [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.