Navier-Stokes solver for hypersonic flow over a slender cone
Author:
Affiliation:
1. Chung Cheng Institute of Technology, Ta-Shi, Taoyuan, Taiwan, Republic of China
2. Armour Research and Development Center, Nan-Tou, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26425
Reference23 articles.
1. Hypersonic wakes and trails
2. An experimental investigation of the near wake of a slender cone at M infinity equal 8 and 12.
3. A study of laminar near wakes.
4. Experimental studies of a laminar hypersonic cone wake.
5. Base pressure measurements on slender cones with domed afterbodies.
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