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Aerodynamic characteristics simulation of simplified debris models from disintegrated reentry spacecraft employing the gas-kinetic unified algorithm

2026/07/28 by Peng Aoping, WU Junlin, Wu Junlin +8
Engineering · Mathematics · #Aerodynamic force #Aerodynamic heating #Aerodynamics #Debris #Gas Dynamics and Kinetic Theory #Reentry #Space Satellite Systems and Control #Spacecraft #Spacecraft Dynamics and Control #Unified Model

paper · doi:10.1016/j.compfluid.2026.107241

openalex publication_date 2026/07/28 · crossref created 2026/07/28 · openalex created_date 2026/07/29 · crossref deposited 2026/08/03 · crossref indexed 2026/08/03 · openalex updated_date 2026/08/04 · crossref issued 2026/10/01 · crossref published 2026/10/01 · crossref published-print 2026/10/01

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