AN INVESTIGATION OF A THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER IN HYPERSONIC FLOW

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1962
Accession Number
AD0294975

Entities

People

  • Gennaro F. Aiello

Organizations

  • New York University Tandon School of Engineering

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Blunt Bodies
  • Boundary Layer
  • Computational Fluid Dynamics
  • Coordinate Systems
  • Equations
  • Flight Speeds
  • Fluid Dynamics
  • Heat Transfer
  • Hypersonic Flight
  • Hypersonic Flow
  • Laminar Boundary Layer
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Three Dimensional Flow
  • Turbulent Boundary Layer

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers