Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Reference8 articles.
1. Van Wie, D., Molder, S.: Application of Busemann inlet designs for flight at hypersonic speeds. 1992 Aerospace Design Conference, Irvine, CA, AIAA Paper 92-1210 (1992). https://doi.org/10.2514/6.1992-1210
2. Molder, S.: A benchmark for in internal flow CFD codes. Comput. Fluid Dyn. J. 12(2), 47–53 (2003)
3. Molder, S.: Curved aerodynamic shock waves. PhD Thesis, McGill University (2012). https://escholarship.mcgill.ca/concern/theses/r781wk88b
4. Moradian, N., Timofeev, E.V., Tahir, R., Molder, S.: On the self-starting constraints for Busemann intakes with overboard spillage. In: Bonazza, R., Ranjan, D. (eds.) Proceedings of 29th International Symposium on Shock Waves, vol. 2, Springer, Cham, pp. 1027–1032 (2015). https://doi.org/10.1007/978-3-319-16838-8_37
5. Moradian, N., Timofeev, E.V., Tahir, R., Molder, S.: Startability analysis of Busemann intakes with overboard spillage. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, AIAA Paper 2014-3227 (2014). https://doi.org/10.2514/6.2014-3227