LAMINAR BOUNDARY LAYER ON A SPINNING CONE AT SMALL ANGLES OF ATTACK

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1956
Accession Number
AD0120099

Entities

People

  • R. Sedney

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Coefficients
  • Computational Science
  • Differential Equations
  • Equations
  • Flow
  • Fluid Dynamics
  • Free Stream
  • Laminar Boundary Layer
  • Mach Number
  • Magnus Effect
  • Molecular Dynamics
  • Prandtl Number
  • Skin Friction
  • Three Dimensional
  • Viscous Flow