A Comparison Between the Drags Predicted by Boundary-Layer Theory and Experimental Drag Data for Bodies of Revolution

Abstract

A finite-difference method used by Wang and Huang to predict the drag coefficients of axisymmetric bodies is systematically applied to eight series of model forms comprising nearly fifty bodies. Calculations of residual drag are compared to available experimental data in order to determine the usefulness of the method for predictive purposes. The method is shown to exhibit little sensitivity to changes in nose or tail radii or prismatic coefficient. The method does exhibit the ability to correctly predict drag trends for variations in length-to-diameter ratio, entrance-length-to-diameter ratio, and tail-length- to-diameter ratio.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1977
Accession Number
ADA046782

Entities

People

  • David W Taylor
  • Nadine M. White

Tags

Communities of Interest

  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Bodies
  • Bodies Of Revolution
  • Boundary Layer
  • Boundary Layer Flow
  • Computational Science
  • Computations
  • Computer Programs
  • Computers
  • Engineering
  • Experimental Data
  • Flow
  • Geometry
  • Layers
  • Mathematics
  • Polynomials
  • Pressure Distribution
  • Ships

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.