Case Study
차세대 엔지니어에게 힘을 실어주는 Ansys
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Case Study
"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
Drag decomposition into profile, induced, and wave drag is a valuable tool for analysis and design of current and future aircraft configurations. Traditionally, drag decomposition is performed in the farfield (e.g., Maskell’s induced drag formula or Oswatitsch’s entropy integral). A novel concept based on partial pressure fields (PPFs) allows for a drag decomposition in the nearfield, thereby providing phenomenological pressure fields as opposed to single-valued integrals.
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 of integration planes. The required software had to be both capable of overset meshes for quantitative comparisons to farfield drag integration and able to supply user-defined Poisson equations to solve for the PPFs.
엔지니어링 과제에 직면하고 있다면우리 팀이 도와드리겠습니다. 풍부한 경험과 혁신에 대한 헌신을 가지고 있는 우리에게 연락해 주십시오. 협력을 통해 엔지니어링 문제를 성장과 성공의 기회로 바꾸십시오. 지금 문의하기