Numerical Simulation of Three-Dimensional High-G Dynamic Maneuvers of a Complete and Flexible Aircraft Configuration

Abstract

Our long term objective is the development of a fast and sound methodology for simulating the dynamic aeroelastic response of an aircraft during three-dimensional high-G maneuvers in transonic and supersonic airstreams. Our focus is on AIR FORCE relevant problems exemplified by a transonic/supersonic lifting body geometry performing complex multi-G maneuvers at a free-stream Mach number M00 ranging between 0.7 and 3 (0.7 </- M(infinity) </- 3).

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1999
Accession Number
ADA384728

Entities

People

  • Charles Farhat

Organizations

  • University of Colorado Boulder

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Applied Mechanics
  • Composite Materials
  • Computational Fluid Dynamics
  • Computational Science
  • Computations
  • Differential Equations
  • Flow
  • Free Stream
  • Fuselages
  • Geometry
  • Lifting Bodies
  • Mach Number
  • Mechanics
  • Simulations
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aviation Science / Aeronautics.
  • Computational Fluid Dynamics (CFD)

Technology Areas

  • Hypersonics