Description and Evaluation of a Digital-Computer Program for Calculating the Viscous Drag of Bodies of Revolution

Abstract

A digital-computer program has been written for calculating the viscous drag of streamlined bodies of revolution in constant-density axial flow. The integral approach adopted incorporates recently improved methods for predicting the transition point and for calculating the turbulent boundary layer. The inputs to the computer program are the body geometry, the associated inviscid pressure distribution, and the body-length Reynolds number. Agreement of calculated and measured drag coefficients is good, particularly in cases where the transition point is predicted accurately.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1975
Accession Number
ADA023995

Entities

People

  • Keith P. Kerney
  • Nadine M. White

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Boundary Layer Transition
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Flow Fields
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Froude Number
  • Geometry
  • Hydrodynamics
  • Integral Equations
  • Plastic Explosives
  • Pressure Distribution
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Fluid Dynamics.