Experimental and Computational Investigation of a Dual-Bell Nozzle
Author:
Affiliation:
1. Worcester Polytechnic Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0377
Reference22 articles.
1. Advanced Rocket Nozzles
2. 3Jones, J. E. 2013. Nanolaunch 1200. NASA-Marshall Space Flight Center
3. Temperature and air–fuel ratio dependent specific heat ratio functions for lean burned and unburned mixture
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