Comparison of DSMC and Experimental Data for Low Reynolds Number Micro-Nozzle
Author:
Affiliation:
1. Naval Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4816
Reference13 articles.
1. Truncated Perfect Nozzles in Optimum Nozzle Design
2. Design of compressed truncated perfect nozzles
3. Exhaust Nozzle Contour for Optimum Thrust
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