| 000 | 00620nam a22001817a 4500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20210308124507.0 | ||
| 008 | 210308b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aMayo, Alton P. | ||
| 245 |
_aMatrix method for obraining spanwise moments and deflections of torsionally rigis rotor blades with arbitrary loadings [Technical Note 4304] _cAlton P. Mayo |
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| 260 |
_aWashington _bNational Advisory Committee for Aeronautics _c1958 |
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| 300 | _a51p | ||
| 440 | _aNational Advisory Committee for Aeronautics (NACA) | ||
| 650 | _amatrix method | ||
| 942 | _cREF | ||
| 999 |
_c564270 _d564270 |
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