Analysis of burst margin and critical speed of gas turbine disc for aeroengine application

Simple item page
dc.contributor.authorKumar, Ranjan
dc.date.accessioned2021-03-12T11:00:45Z
dc.date.available2021-03-12T11:00:45Z
dc.date.issued2021-03
dc.identifier.urihttp://hdl.handle.net/123456789/1937
dc.language.isoenen_US
dc.publisherIndian Institute of Technology (Indian School of Mines), Dhanbaden_US
dc.subjectGas turbine discen_US
dc.subjectBurst speeden_US
dc.subjectAircraft gas turbine engineen_US
dc.subjectBurst marginen_US
dc.subjectPh.Den_US
dc.subjectMECHen_US
dc.subjectPH1727en_US
dc.titleAnalysis of burst margin and critical speed of gas turbine disc for aeroengine applicationen_US
dc.typeThesisen_US
Files
Original bundle
Now showing 1 - 2 of 2
Thumbnail Image
Name:
Abstract.pdf
Size:
23.72 KB
Format:
Adobe Portable Document Format
Description:
Download
Thumbnail Image
Name:
PH1727.pdf
Size:
5.96 MB
Format:
Adobe Portable Document Format
Description:
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed upon to submission
Description:
Download
Collections
Sanjoy Kumar Ghoshal