000 00602nam a2200181 4500
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