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PARAMETRIC STUDY OF THE EFFECT OF BLADE SHAPE ON THE PERFORMANCE OF TURBOMACHINERY CASCADES: PART III A: AERODYNAMIC DAMPING BEHAVIOUR – COMPRESSOR PROFILES
KTH, School of Industrial Engineering and Management (ITM), Energy Technology, Heat and Power Technology.
2010 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Place, publisher, year, edition, pages
2010. , 143 p.
Series
EGI 2010: 088
Keyword [en]
flutter, turbomachinery, aeroelasticity, compressor
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-131210OAI: oai:DiVA.org:kth-131210DiVA: diva2:654950
Educational program
Master of Science - Aerospace Engineering
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Examiners
Available from: 2013-10-30 Created: 2013-10-09 Last updated: 2013-10-30Bibliographically approved

Open Access in DiVA

MSc Thesis - Lucio Monaco(5577 kB)631 downloads
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File name FULLTEXT01.pdfFile size 5577 kBChecksum SHA-512
a4638a4b458f09b85a4c40d74b9e14c3955fda79974dcedc7c2e79e8ef5abb535eedac61b215563e0f73beb86774de08171e195e6cf07f210d455b190e08005a
Type fulltextMimetype application/pdf

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