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

reportActive / Technical Report | Accession Number: ADA515596 | Open PDF

Abstract:

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

Author(s):
Schiavetta, L. A. ; Cummings, R. M. ; Boelens, O. J. ; Fritz, W.
Author Organization(s):
GLASGOW UNIV (UNITED KINGDOM) DEPT OF AEROSPACE ENGINEERING
Descriptive Note:
Briefing charts
Supplementary Note:
Presented at the International Symposium on Integrating CFD and Experiments in Aerodynamics (3rd), USAF Academy, Colorado Springs, CO on 20-21 Jun 2007. Prepared in collaboration with the United States Air Force Academy, Colorado Springs, CO; NRL, Netherlands; and EADS, Germany. The original document contains color images.
Pagination:
0027

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Monitor Series:
AFOSR
 Subject Terms
Joint Capability Areas:
JCA_6_Net Centric; JCA_8_Building Partnerships
Communities of Interest:
Space
Descriptor(s):
*COMPUTATIONAL FLUID DYNAMICS, *TRANSONIC FLOW, UNITED KINGDOM, DELTA WINGS, SYMPOSIA, PRESSURE GRADIENTS
Field(s)/Group(s):
Fluid Mechanics
Keyword(s):
SHOCK VORTEX INTERACTION, BRIEFING CHARTS, FOREIGN REPORTS, CRITICAL ANGLES
Report Date:
2007 Jun 01
Creation Date:
2010 Mar 24