DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
ADA191494
Title:
Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers.
Corporate Author:
PRINCETON UNIV NJ DEPT OF MECHANICAL AND AEROSPACE ENGINEERING
Report Date:
1988-01-21
Abstract:
This three-year contract originally had two tasks to investigate the structure of flat plate supersonic turbulent boundary layers Task A, and to investigate longitudinal curvature effects in turbulent boundary layers Task B. As a result of the work performed under these task headings, we identified a need to study the structure of simple, wall-bounded vortex loops. This investigation Task C commenced in the third year, and we feel that it has made a major contribution to our understanding of the ensemble-averaged structure of low and high speed turbulent boundary layers. The progress reported here is that achieved in completing these three tasks. Keywords Turbulent flow EddiesFluid mechanics Flow visualization.
Descriptive Note:
Final rept. Jan 85-Jan 88,
Supplementary Note:
DOI: 10.21236/ADA191494
Pages:
0038
Contract Number:
AFOSR-85-0126
File Size:
1.66MB
