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

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1963
Accession Number
AD0403486

Entities

People

  • Gennaro F. Aiello

Organizations

  • New York University Tandon School of Engineering

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Coordinate Systems
  • Equations
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Hypersonic Flow
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Stagnation Point
  • Stagnation Pressure
  • Turbulent Boundary Layer

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers