Parametric dependencies of aeroengine flutter for flutter clearance applications /
This thesis describes the effects of operational parameters upon aeroengine flutter stability. The study is composed of three parts: theoretical development of relevant parameters, exploration of a computational model, and analysis of fully scaled test data. Results from these studies are used to de...
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| Format: | Book |
| Language: | English |
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Cambridge, Mass. :
Gas Turbine Laboratory, Massachusetts Institute of Technology,
[2000]
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| Series: | GTL report ;
#231 |
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Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Massachusetts Institute of Technology
| Call Number: |
TJ778.M41.G24 no.231 |
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