Hypersonic Experimental and Computational Capability, Improvement and Validation. Volume 2. (l'Hypersonique experimentale et de calcul - capacite, ameliorafion et validation)

Abstract

Partial contents include: (1) Shock Wave Boundary Layer Interactions in High Mach Number Flows: A Critical Survey of Current Numerical Prediction Capabilities; (2) Hypersonic Laminar-Turbulent Transition; (3) Real Gas / Blunt Cone Phase II Report; (4) Extrapolation from Wind Tunnel to Flight: Shuttle Orbiter Aerodynamics; (5) Real-Gas Aerothermodynamics Test Facilities.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1998
Accession Number
ADA360865

Entities

People

  • Ajay Kumar
  • Christian Dujarric
  • Jean Muylaert

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Hydrodynamics
  • Hypervelocity Flow
  • Measurement
  • Monte Carlo Method
  • Physics Laboratories
  • Pressure Distribution
  • Pressure Measurement
  • Test And Evaluation
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.
  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Space
  • Space - Hall-Effect Thruster