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All issues Volume 304 (2019) MATEC Web Conf., 304 (2019) 03001 References
Open Access
Issue
MATEC Web Conf.
Volume 304, 2019
9th EASN International Conference on “Innovation in Aviation & Space”
Article Number 03001
Number of page(s) 8
Section Propulsion & Engines
DOI https://doi.org/10.1051/matecconf/201930403001
Published online 17 December 2019
  1. Roncioni, P., Natale, P., Marini, M., Langener, T., & Steelant, J. (2013, September). Numerical simulations of the LAPCAT MR-2 vehicle scramjet engine. In 21st International Symposium Air Breathing Engines, ISABE-2013-1656, American Institute of Aeronautics and Astronautics. [Google Scholar]
  2. Steelant, J., Langener, T., Flight, H., Engine, C. C., & Ramjet, D.M. (2014). The LAPCAT-MR2 hypersonic cruiser concept. ratio, 2, 2. [Google Scholar]
  3. Steelant, J. (2011, April). Sustained hypersonic flight in Europe: first technology achievements within LAPCAT II. In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (p. 2243). [Google Scholar]
  4. Fernández Villacé, V. (2013). Simulation, Design and Analysis of Air-Breathing Combined-Cycle Engines for High Speed Propulsion (Doctoral dissertation, Aeronauticos). [Google Scholar]
  5. Fernández Villacé, V. & Paniagua, G. (2010). Simulation of a combined cycle for high speed propulsion. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (p. 1125). [Google Scholar]
  6. Moral, J., Pérez Vara, R., Steelant, J., & De Rosa, M. (2010). ESPSS simulation platform. Space Propulsion. [Google Scholar]
  7. Verstraete, T. (2010, September). CADO: a computer aided design and optimization tool for turbomachinery applications. In 2nd Int. Conf. on Engineering Optimization, Lisbon, Portugal, September (pp. 6–9). [Google Scholar]
  8. Micka, D. J., Driscoll, J.F.& (2009). Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder. Proceedings of the combustion institute, 32(2), 2397–2404. [Google Scholar]
  9. Torrez, S., Scholten, N., Micka, D., Driscoll, J., Bolender, M., Doman, D., & Oppenheimer, M. (2008, July). A scramjet engine model including effects of precombustion shocks and dissociation. In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (p. 4619). [Google Scholar]
  10. EcosimPro. Modelling a Simulation Software. Installation & Getting Started Guide. Version 5.2. Madrid, EA International. [Google Scholar]
  11. Petzold, L.R. (1982). Description of DASSL: a differential/algebraic system solver (No. SAND-82-8637; CONF-820810-21). Sandia National Labs., Livermore, CA (USA). [Google Scholar]
  12. Fernández-Villace, V., Paniagua, G., & Steelant, J. (2014). Installed performance evaluation of an air turbo-rocket expander engine. Aerospace science and technology, 35, 63–79. [Google Scholar]
  13. Meerts, C., Steelant, J., & Hendrick, P. (2011, May). Preliminary design of the low speed propulsion air intake of the LAPCAT-MR2 aircraft. In 7th European Symposium on Aerothermodynamics, number ESA-SP-692 in ESA Special Publications, European Space Agency. [Google Scholar]
  14. Churchill, S. W., & Usagi, R. (1972). A general expression for the correlation of rates of transfer and other phenomena. AIChE Journal, 18(6), 1121–1128. [Google Scholar]
  15. Heiser, W. H., & Pratt, D.T. (1994). Hypersonic airbreathing propulsion. Aiaa. [Google Scholar]
  16. Ispir, A. C., & Saracoglu, B.H. (2019). Development of a 1D dual mode scramjet model for a hypersonic civil aircraft. In AIAA Propulsion and Energy 2019 Forum (p. 3842). [Google Scholar]
  17. O'Brien, T.F., & Starkey, R. P., Lewis, M.J. (2001). Quasi-one-dimensional high-speed engine model with finite-rate chemistry. Journal of propulsion and power, 17(6), 1366–1374. [Google Scholar]
  18. Riehmer, J., & Gü lhan, A. (2011, May). Design of a Scramjet Nozzle with Streamline Tracing Technique and Reference Temperature Method. In 7th Aerodynamics Symposium on Space Vehicles. [Google Scholar]
  19. Piscitelli, F., Cutrone, L., Pezzella, G., Roncioni, P., & Marini, M. (2017). Nose-to-tail analysis of an airbreathing hypersonic vehicle using an in-house simplified tool. Acta Astronautica, 136, 148–158. [Google Scholar]
  20. Goncalves, P. M., Ispir, A. C., & Saracoglu, B.H. (2019). Development and optimization of a hypersonic civil aircraft propulsion plant with regenerator system. In AIAA Propulsionand Energy 2019 Forum (p. 4421). [Google Scholar]

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