Three-Dimensional Test Experience with a Transonic Adaptive-Wall Wind Tunnel.

Abstract

A square 9-inch wind tunnel with solid sidewalls and flexible upper and lower rod walls capable of 3-D contouring was used to test an axisymmetric and a winged lifting model at M=0.50 to 0.95. The simple, direct analytical method for wall contouring uses the model geometry for solid blockage and iterative model force data to adapt for lift and for wake blockage. Solid sidewall effects and the convergence of the adaptation scheme are evaluated. Linear and nonlinear theory for solid blockage is compared. Interesting comparisons are also made between 2-D and 3-D wall contouring. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1983
Accession Number
ADA129858

Entities

People

  • Donald J. Harney

Organizations

  • University of Dayton

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computer Programs
  • Engineering
  • Fluid Dynamics
  • Geometry
  • Instrumentation
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Test And Evaluation
  • Three Dimensional
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Dynamics.