The Birth of Open Separation on a Prolate Spheroid

Abstract

Results are presented to describe the laminar flow patterns around a prolate spheroid at angles of attack of 1, 2, 3, and 30 degrees and complement those obtained previously at 6 degrees. They were obtained by solving three- dimensional boundary-layer equations with a combination of standard and characteristic box methods and with a stability criterion to ensure numerical accuracy. Emphasis is placed on the nature of separation which , in agreement with experiment but contrary to some theoretical claims, is shown to be open for all angles of attack and to be coincident with a particular skin friction line. Keywords: Fluid mechanics, Boundary layers, Bodies of revolution, Crossflow, Singularity, Three-dimensional flows.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1988
Accession Number
ADA201350

Entities

People

  • Tuncer Cebeci
  • Wenhan Su

Organizations

  • McDonnell Douglas

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Aircrafts
  • Bodies
  • Boundary Layer
  • Equations
  • Flow
  • Fluid Dynamics
  • Fluid Mechanics
  • Friction
  • Laminar Flow
  • Layers
  • Scientific Research
  • Skin Friction
  • Standards
  • Three Dimensional
  • Three Dimensional Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Systems Analysis and Design