Adaptive Meshing of Ship Air-Wake Flowfields

Abstract

Numerical simulations of aircraft landing on a carrier are difficult due to complex geometry and complex flow physics. The flowfield is very unsteady and chaotic and adequate mesh resolution is crucial to a successful simulation. The goal of the proposed research is to deliver enhanced mesh adaptation capabilities that account for the chaotic unsteady nature of the flowfield about an aircraft in the landing approach path. Similar work was published by Shipman, et. al. [Shipman, Arunajatesan, Cavallo, Polsky] The objectives of the research are to explore three distinct mesh adaptation methods to handle the dynamic aspect of this case. The three methods include a hierarchical-Cartesian hexahedral method, an all-tetrahedral mesh method and a physics-based point placement/meshless method. The hierarchical method will subdivide cube-shaped elements to resolve geometry and gradients of user-selected adaptation functions, such as pressure or Mach number. The tetrahedral method is a traditional unstructured mesh method that incorporates adaptation through node movement to resolve gradients of the adaptation function. The third method is a meshless method that uses a physics-based force model to move nodes around to resolve the geometry and flowfield. The initial phase of the research conducted the first year developed steady-state analysis procedures for each method, with appropriate mesh adaptation capabilities. A description of the steady-state version of the three computer codes (TetFlow, OctFlow and PointFlow) is described in this report. The outcome of the research will provide insight into efficient and robust approaches for adaptive meshing for dynamic simulation of aircraft landings in the presence of unsteady carrier flowfield. Research is conducted assuming inviscid flow, but approaches will be applicable to viscous simulations with modifications.

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Document Details

Document Type
Technical Report
Publication Date
Oct 21, 2014
Accession Number
ADA613622

Entities

People

  • Steve Karman

Organizations

  • University of Tennessee system

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aircraft Landings
  • Computational Fluid Dynamics
  • Equations
  • Equations Of Motion
  • Euler Equations
  • Flow
  • Fluid Dynamics
  • Geometry
  • Inviscid Flow
  • Mach Number
  • Point Clouds
  • Pressure Gradients
  • Simulations
  • Steady State
  • Students
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Wave Propagation and Nonlinear Chaotic Dynamics.