An edge-based solution-adaptive method applied to the AIRPLANE code - Info and Reading Options
By Rupak Biswas
“An edge-based solution-adaptive method applied to the AIRPLANE code” Metadata:
- Title: ➤ An edge-based solution-adaptive method applied to the AIRPLANE code
- Author: Rupak Biswas
“An edge-based solution-adaptive method applied to the AIRPLANE code” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Transonic flow - Near fields - Unstructured grids (Mathematics) - Flow distribution - Aircraft configurations - Sonic booms - Grid generation (Mathematics) - Supersonic flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL11565404W
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