Optimization of Low-Drag Bodies of Revolution with Turbulent Boundary Layers.

Abstract

Numerical optimization methods are used to search for minimum-drag bodies of revolution in incompressible flow with all-turbulent boundary layers. Available methods for potential flow, boundary layer, drag, and optimization calculations are used. Results obtained with an empirical drag formula give a low-fineness ratio body with significantly lower drag than for traditional shapes. However, when the drag method of Nakayama and Patel is used as a representative state-of-the-art capability, results show that the drag is insensitive to perturbations from the shape of traditional bodies, and only a small reduction in drag is obtained. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1977
Accession Number
ADA041313

Entities

People

  • E. M. Murman
  • Edward W. Geller
  • John E. Mercer
  • Ralph W. Metcalfe

Tags

Communities of Interest

  • Counter IED
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Bodies Of Revolution
  • Boundary Layer
  • Boundary Layer Transition
  • Computer Programs
  • Drag
  • Fineness Ratio
  • Flow Fields
  • Friction
  • Hydrodynamics
  • Incompressible Flow
  • Layers
  • Mechanical Engineering
  • Pressure Distribution
  • Pressure Gradients
  • Stratified Fluids
  • Turbulent Boundary Layer
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design