Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
Cranfield University
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Output 0 of 0 in the submission
Article title
Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation
Type
D - Journal article
DOI
-
Title of journal
The Aeronautical Journal
Article number
-
Volume number
114
Issue number
1155
First page of article
299
ISSN of journal
0001-9240
Year of publication
2010
URL
-
Number of additional authors
5
Additional information
This work was sponsored by the Indian Government through the Indian Defence Research and Development Laboratory under contract DRDL/33/96P/05/0750/31824 (value £70k). The programme was designed to improve understanding of aero-thermal effects on launch vehicles and to improve semi-empirical prediction methods particularly in relation to localised effects (and as a result structural integrity) caused by surface excressecences at the freestream Mach numbers experienced during a typical trajectory to earth orbit, contact Dr Panneerselvam Subramanian (hyd2_panneers@yahoo.co.in)
Interdisciplinary
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Cross-referral requested
-
Research group
E - Sensors and Measurement Science
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
