Multidisciplinary Shape Optimization of Missile Fin Configuration Subject to Aerodynamic Heating
Author:
Affiliation:
1. University of Belgrade, 11000 Belgrade, Serbia
2. UNION–Nikola Tesla University, 11000 Belgrade, Serbia
3. City Administration of the City of Belgrade, 11000 Belgrade, Serbia
Funder
Ministarstvo Prosvete, Nauke i Tehnološkog Razvoja
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference63 articles.
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4. Effect of Mach number on thermoelectric performance of SiC ceramics nose-tip for supersonic vehicles
5. Highly cited literature of high-speed compressible flow research
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