Oscillating 65 Deg. Delta Wing, Experimental

Abstract

This data set contains force and pressure data resulting from static and dynamic measurements on a sharp-edged cropped delta wing with a leading edge sweep of 65 oscillating in different modes. Motivation for the experiment were the provision of experimental data for validation of unsteady computational codes and understanding of the flow past an oscillating delta wing. The model geometry is identical to a geometry used in the Vortex Flow Experiment for Computer Code Validation (VFE), a multinational cooperation which provided experimental data of delta wing configurations in the mid eighties 3, 4 The geometry of the wing is also used for steady and unsteady calculations within the Western European Armament Group (WEAG, formerly lEP(3)TA- ii.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 2000
Accession Number
ADP010725

Entities

People

  • Thomas Loeser

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Analysis Of Variance
  • Boundary Layer
  • Data Sets
  • Delta Wings
  • Dynamic Pressure
  • Experimental Data
  • Experimental Design
  • Fourier Analysis
  • Frequency
  • Geometry
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Statistical Analysis
  • Transducers
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • European Security and Defence Policy (ESDP).
  • Fluid Mechanics and Fluid Dynamics.