Sting Influence on Vortex Breakdown on a 65 Degree Delta Wing in Transonic Flow

Abstract

Study compared various computational fluid dynamics outcomes for sharp delta wings.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2007
Accession Number
ADA515596

Entities

People

  • L. A. Schiavetta
  • O. J. Boelens
  • R. M. Cummings
  • W. Fritz

Organizations

  • University of Glasgow

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Axial Flow
  • Computational Fluid Dynamics
  • Delta Wings
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Mach Number
  • Measurement
  • Pressure Gradients
  • Pressure Measurement
  • Transonic Flow
  • United States
  • United States Air Force Academy

Fields of Study

  • Physics