The Validation of the WL/FIM Trisonic Gasdynamic Facility for Exhaust Nozzle Testing

Abstract

The Wright Laboratory's expanding requirement for reliable resident exhaust nozzle testing capability necessitated the verification of the experimental capability of the Trisonic Gasdynamics Facility (TGF) located at Wright-Patterson Air Force Base. A validation test, directed toward the TGF's nozzle testing capability, compared surface pressure data taken from an axisymmetric AGARD reference nozzle from a wind tunnel test performed at the Propulsion Wind Tunnel (PWT) at Arnold Engineering Development Center (AEDC). Boattail pressure distributions and pressure drag measurements were compared between the facilities. Cross-sectional blockage caused significant differences between boattail pressures and pressure drag coefficients between facilities. Computational fluid dynamics (CFD) tools were used to aid understanding of differences found in the comparison study. A series of CFD simulations aimed at determining the actual freestream flow Mach number is recommended to improve flow simulating accuracy in the TGF.... Wind tunnel, Simulation, Drag, Validation, Boattail, Computational Fluid Dynamics(CFD), Pressure coefficient, Blockage

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1992
Accession Number
ADA266238

Entities

People

  • Robert D. Gillgrist

Organizations

  • Wright Laboratory

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Air Force Facilities
  • Computational Fluid Dynamics
  • Exhaust Nozzles
  • Experimental Data
  • Fluid Dynamics
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Simulations
  • Static Pressure
  • Test Facilities
  • Three Dimensional
  • Validation
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computational Modeling and Simulation
  • Fluid Dynamics.