000 | 00604 a2200157 4500 | ||
---|---|---|---|
005 | 20221207124000.0 | ||
100 | _aPinckney, S. Z. | ||
245 | 1 |
_aNASA TM [X-1110] _bUSE OF A SINGLE TURNING VANE TO ELIMINATE FLOW SEPERATION IN A SPACE-LIMITED 90(DEGREE) INTAKE ELBOW OF AN AXIAL-FLOW COMPRESSOR _cS. Z. Pinckney |
|
260 |
_aWashington _bNational Aeronautics and Space Administration _c1965 |
||
300 | _a28p | ||
440 | _aNASA Technical Memorandum | ||
490 | _aX-1110 | ||
500 | _aTechnical Memorandum X-1105-1123 Bound Vol. No.102490; Contents: TR-7988-7992 | ||
650 | _aAeronautics | ||
942 | _cTR | ||
999 |
_c393011 _d393011 |