Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Judy Odam"'
Publikováno v:
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::42c92424a20313713767ec21c314744a
https://doi.org/10.2514/6.2011-2356
https://doi.org/10.2514/6.2011-2356
Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::188b2e8ee136a8cdeb0ae207925680f6
https://doi.org/10.2514/6.2009-7265
https://doi.org/10.2514/6.2009-7265
Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
The objective of the Hypersonic International Flight Research Experimentation (HIFiRE) program is to increase understanding of fundamental hypersonic phenomena and to develop technologies deemed critical to the realization of next generation aerospac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::938919e0c072b3dfcc25b9ab7fe0cca0
https://doi.org/10.2514/6.2009-7293
https://doi.org/10.2514/6.2009-7293
Publikováno v:
AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference.
Computational fluid dynamics simulations are a valuable tool in validating a scramjet design prior to expensive flight testing. However, the number of conditions that need to be analysed in order to piece together a flight trajectory combined with th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7297a6d2ed14aa2c1edad4520f5d15fb
https://doi.org/10.2514/6.2005-3338
https://doi.org/10.2514/6.2005-3338
Publikováno v:
Scopus-Elsevier
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6ffcd38148979ce45cb17268e745a69e
https://doi.org/10.2514/6.2005-3339
https://doi.org/10.2514/6.2005-3339
Autor:
Judy Odam, Allan Paull
Publikováno v:
12th AIAA International Space Planes and Hypersonic Systems and Technologies.
Pressure measurements were taken along the intake, combustion chamber and thrust surface of a scram-jet model tested in a free-piston driven shock tunnel. The scramjet model incorporated a single rectangular cross-section combustion chamber of consta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df92c3eee59083fa2f14d6407c7808f0
https://doi.org/10.2514/6.2003-6961
https://doi.org/10.2514/6.2003-6961