ESTIMATION OF DEVIATION ANGLE FOR AXIAL-FLOW COMPRESSOR BLADE SECTIONS USING INVISCID-FLOW SOLUTIONS
By: Miller,Max J.
Material type:![materialTypeLabel](/opac-tmpl/lib/famfamfam/BK.png)
Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
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PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-7549 - (Browse shelf) | Not for loan | TR8390 |
Total holds: 0
Bound With Nasa Tn D-7541-50
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