RDHWT/MARIAH II Hypersonic Wind Tunnel Research Program

Abstract

The U.S. Air Force sponsored and the USAF Arnold Engineering Development Center directed the Radiantly Driven Hypersonic Wind Tunnel (RDHWT)/ Magnetohydrodynamic Accelerator Research Into Advanced Hypersonics (MARIAH II) Program. This report primarily covers the research for the period from January 2001 through July 2004. The scope of the research program was to develop enabling technologies for a medium-scale hypersonic wind tunnel (MSHWT) that would provide a Mach 8 to 15 test capability with aeropropulsion testing as the principal need and focus. The USAF research program has been terminated, but work continues under Army sponsorship. Considerable progress has been achieved, and this final report summarizes the work. Key participants in this work were MSE Technology Applications, Inc., the prime integrating contractor; Princeton University; Ring Technical Services (RTS); Lawrence Livermore National Laboratory (LLNL); Sandia National Laboratory (SNL); and Oak Ridge National Laboratory (ORNL) (funded by a separate DoD program).

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 2008
Accession Number
ADA487128

Entities

People

  • C. C. Limbaugh
  • J L Jordan
  • M. L. Laster

Tags

Communities of Interest

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

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Chemistry
  • Computational Fluid Dynamics
  • Electric Arcs
  • Energy Transfer
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Material Degradation Processes
  • Pressure Distribution
  • Pressure Measurement
  • Test And Evaluation
  • Test Facilities
  • Thermodynamics
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Marine Propulsion Engineering and Naval Architecture
  • Research Science/Academic Research

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow