Pre-Flight Ground Testing of the Full-Scale HIFiRE-1 at Fully Duplicated Flight Conditions

Abstract

As part of an experimental study to obtain detailed heating and pressure data over the full-scale HIFiRE-1 flight geometry, CUBRC has completed a 30-run matrix of ground tests, sponsored by the AFOSR, to determine the optimal flight hardware and instrumentation configuration necessary to achieve and make measurements of desired flow phenomena during the flight experiment HIFiRE-1 stands for Hypersonic International Flight Research and Experimentation and the flight vehicle consists of a blunt nose, cone cylinder, and flare regions. The primary objective of the HIFiRE-1 flight experiment is to collect high quality flight data to be used for CFD code and ground test facility validation in regions of boundary layer transition as well as regions of separated shock wave/boundary layer interaction at the cylinder/flare junction.

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Document Details

Document Type
Technical Report
Publication Date
May 14, 2008
Accession Number
ADA481826

Entities

People

  • Erik Mundy
  • Matthew G. Maclean
  • Michael S. Holden
  • Tim P. Wadhams

Organizations

  • Calspan-University of Buffalo Research Center

Tags

Communities of Interest

  • Air Platforms
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Boundary Layer Transition
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Fluid Mechanics
  • Geometry
  • Heat Transfer
  • Instrumentation
  • Measurement
  • Physics Laboratories
  • Pressure Gages
  • Pressure Measurement
  • Shock Tunnels
  • Shock Waves
  • Test Facilities
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

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