1 “Ansys Fluent allowed us to implement, verify, and validate the theory of using partial pressure fields (PPFs) for aircraft drag decomposition which has the potential to improving our collective understanding of the various sources of drag and their interference.” Sven Schmitz Boeing / A.D Welliver Professor / The Pennsylvania State University Ansys + Penn State University CASE STUDY /A Near-Field Drag Decomposition Using Ansys Fluent Poisson Solver // 2 A Nearfield Drag Decomposition Using Ansys Fluent Poisson Solver / Challenges The long-term goal is to have a reliable means of aircraft drag decomposition that applies equally to current and future aircraft configurations (e.g., blended wing-body, integrated propulsion systems, etc.) and is unambiguous to the particular choice

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