Design of Optimized Two-Dimensional Scramjet Nozzle Contour for Hypersonic Vehicle Using Evolutionary Algorithms
Author:
Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-46213-4_19
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3. Huang, W., et al.: Design exploration for a single expansion ramp nozzle (SERN) using data mining. Acta Astronaut. 83, 10–17 (2013)
4. Ogawa, H., Boyce, R.R.: Physical insight into nozzle flow behaviour of axisymmetric scramjets for access-to-space via design optimisation. In: Australian Space Science Conference 2010. National Space Society of Australia (2010)
5. www.sandi.co.in/
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