000 | 00602nam a2200181 4500 | ||
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003 | OSt | ||
005 | 20220107121057.0 | ||
008 | 220107b xxu||||| |||| 00| 0 eng d | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
100 | _aBorst, Henry V. | ||
245 |
_aA new blade element method for calculating the performance of high intermediate solidity axial flow fans [NASA TR-3063] _cHenry V. Borst |
||
260 |
_aWashington, D. C. _bNational Aeronautics and Space Administration _c1978 |
||
300 | _a48p | ||
440 | _aNational Aeronautics and Space Administration | ||
650 | _aAxial flow | ||
942 | _cREF | ||
999 |
_c565305 _d565305 |