Numerical Investigation of High-Enthalpy Flows Generated by Expansion Tube
Author:
Affiliation:
1. Shizuoka University, Hamamatsu 432-8561, Japan
2. Institute of Space and Astronautical Science, Sagamihara 229-8510, Japan
3. Tohoku University, Sendai 980-8577, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1610
Reference22 articles.
1. Sample and return mission from asteroid Nereus via solar electric propulsion
2. Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders
3. Fully coupled implicit method for thermochemical nonequilibrium air at suborbital flight speeds
4. Effective Test Time Evaluation in High-Enthalpy Expansion Tube
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