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:
ADA614100
Title:
Investigation of Optimal Numerical Methods for High Reynolds Number Unsteady Simulations (Briefing Charts)
Descriptive Note:
Corporate Author:
AIR FORCE RESEARCH LAB EDWARDS AFB CA ROCKET PROPULSION DIV
Report Date:
2014-04-12
Pagination or Media Count:
15.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE