Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
Cranfield University
Return to search
Output 0 of 0 in the submission
Article title
Measurement of shock wave unsteadiness using a high-speed schlieren system and digital image processing
Type
D - Journal article
Title of journal
Review of Scientific Instruments
Article number
-
Volume number
79
Issue number
12
First page of article
126108-1
ISSN of journal
0034-6748
Year of publication
2008
URL
-
Number of additional authors
4
Additional information
The techniques outlined in this paper were adapted to support wind tunnel tests on an EPSRC funded collaborative project with Southampton, Cambridge and Manchester Metropolitan Universities: 'A Study of Practical Abatement Techniques for Exhaust Jets from Commercial Aircraft'. (EP/H002987/1). This has led to a novel technique for vortex wake simulation, to more accurately simulate vortex dynamics and hence pollutant dispersion.
Interdisciplinary
-
Cross-referral requested
-
Research group
A - Aerospace Engineering
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
