Computational Analysis of High-Speed Ejection Seats

Abstract

This final report documents the results of a study demonstrating the use of analytical computational fluid dynamics methods to predict the aerodynamic characteristics and flowfield details of a typical ejection seat with an occupant. This feasibility study was limited to two dimensional flow around a configuration defined by a longitudinal plane of symmetry through the center of the ejection seat. Navier-Stokes codes were used to predict the steady and time-dependent transonic and supersonic flow characteristics for a series of ejection seats for which wind tunnel data are available, and comparisons of measured and predicted forces and moments are presented to show the trends produced by the analysis techniques. Structured and unstructured grids were considered in the calculations to demonstrate the capability of the method and to guide the planning for a future three-dimensional approach. The report concludes with recommendations for a program leading to the development of a three-dimensional CFD analysis code applicable to the study of windblast loads and minimum drag design of modern ejection seats. (AN)

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Document Details

Document Type
Technical Report
Publication Date
Apr 20, 1991
Accession Number
ADA290328

Entities

People

  • Michael R. Mendenhall
  • Steven C. Caruso

Organizations

  • Nielsen Engineering & Research (United States)

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Differential Equations
  • Feasibility Studies
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Geometry
  • Mechanical Properties
  • Pressure Distribution
  • Three Dimensional
  • Turbulent Mixing
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computational Modeling and Simulation
  • Explosive Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow