| 000 | 01089 a2200289 4500 | ||
|---|---|---|---|
| 001 | 375189 | ||
| 003 | OSt | ||
| 005 | 20220827151738.0 | ||
| 008 | 201202b ||||| |||| 00| 0 eng d | ||
| 040 | _cIITB | ||
| 041 | _aeng | ||
| 080 |
_a043:533.6.01:518.6 _bAlo |
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| 100 |
_aAlone, Dilipkumar Bhanudasji _918757 _eAuthor |
||
| 245 | _aEnhancing the stability margin of single stage transonic axial flow compressor with bend skewed casing treatment (R) | ||
| 260 |
_aBombay _bIIT _c2015 |
||
| 300 |
_axxiv,285 p. _c30 cm |
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| 502 |
_aThesis _bPh.D. _cIndian Institute of Technology Bombay. Department of Aeronautical Engineering _d2015 |
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| 650 | 0 |
_aTheses and Dissertations _921 |
|
| 650 |
_aAxial flow compressors _xAerodynamics _918751 |
||
| 650 | 0 |
_aCascades(Fluid dynamics) _918758 |
|
| 650 | 0 |
_aNumerical analysis _9426 |
|
| 700 |
_aPradeep, A.M. _eSupervisor _910225 |
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| 700 |
_aRamamurthy, S. _eSupervisor _928173 |
||
| 700 |
_aIyengar,Venkat S. _928174 |
||
| 710 |
_aIndian Institute of Technology Bombay _bDepartment of Aeronautical Engineering _9401 |
||
| 942 |
_cTD _2udc |
||
| 999 |
_c236341 _d236341 |
||