Skip to Main Content
Free Trials

 

Case Study

Penn State University Finds Reliable Means of Aircraft Drag Decomposition

"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

Introduction

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.

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 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.

Engineering Solution

  • High-quality structured meshes provide verification and validation• User-defined scalars are easy to implement.
  • Ansys Fluent user-defined functions (UDF) package allows for an unparalleled degree of customization.
  • The unique capability of an available Poisson solver within user-defined transport equations is included.
  • Overset meshing allows for farfield drag decomposition to be conducted concurrent with nearfield PPF decomposition.

Benefits

  • Ansys Fluent enabled simultaneous nearfield and farfield drag decomposition.
  • The inclusion of a 3D Poisson solver within Fluent is unique and is not commonly available in other commercial CFD packages.
  • Ansys Fluent was critical to NASA University Leadership Initiative (ULI) research on ultra-efficient commercial aircraft.