Proceedings of the Boundary Layer Transition Workshop Held 3-5 November 1971. Volume 3

Abstract

Contents: Effects of Mass Addition Distribution and Roughness on Boundary Layer Transition at Mach 12; Effects of Nose Bluntness and Free-Stream Unit Reynolds Number on Slender Cone Transition at Hypersonic Speeds; Free Flight Determination of Boundary Layer Transition on Small Scale Cones in the Presence of Surface Ablation; Effects of Wall Cooling and Angle of Attack on Boundary-Layer Transition on Sharp Cones at Free Stream Mach no. = 7.4; Some Special Features of Boundary Layer Transition on Aeroballistic Range Models; Hypersonic Simulation for Lifting Body Transition Studies; Effect of Transition on Three-Dimensional Shock Wave-Boundary Layer Interaction; Hypersonic Shock Tunnel Transition Studies; Open Questions - Transition to Turbulence at High Speeds; and Lessons from Transition of Shock-Tube Boundary Layers.

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Document Details

Document Type
Technical Report
Publication Date
Dec 20, 1971
Accession Number
AD0909223

Entities

People

  • W. D. Mccauley

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Air Platforms
  • Cyber
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Control
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Visualization
  • Fluid Dynamics
  • Geometry
  • Hydrodynamics
  • Jet Propulsion
  • Measurement
  • Pressure Distribution
  • Surface Properties
  • Test And Evaluation
  • Test Facilities
  • Three Dimensional
  • Turbulent Mixing
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow