Return to search

Hypersonic aerospace vehicle leading edge cooling using heat pipe, transpiration and film cooling techniques

No description available.
Identiferoai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/16347
Date08 1900
CreatorsModlin, James Michael
PublisherGeorgia Institute of Technology
Source SetsGeorgia Tech Electronic Thesis and Dissertation Archive
Detected LanguageEnglish
TypeDissertation
RightsAccess restricted to authorized Georgia Tech users only.

Page generated in 0.0083 seconds