| 000 | 00627nam a2200181 4500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20220705105156.0 | ||
| 008 | 220705b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aPinckney, S. Z. | ||
| 245 |
_aUse of a single turning vane to eliminate flow separation in a space limited 90 degree intake elbow of an axial flow compressor [NASA TM X-1110] _cS. Z. Pinckney |
||
| 260 |
_aWashington, D. C. _bNational Aeronautics and Space Administration _c1965 |
||
| 300 | _a28p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 650 | _aAxial flow | ||
| 942 | _cREF | ||
| 999 |
_c565793 _d565793 |
||