DIFFERENTIAL ANALYSIS FOR THE TURBULENT BOUNDARY LAYER ON A COMPRESSOR BLADE ELENMENT (INCLUDING BOUNDARY-LAYYER SEPARATION)
By: Schmidt,James F.
Contributor(s): Todd,Carroll A.
Material type:
BookPublisher: Nasa, Washington, D.C. 1974Description: 28.DDC classification: NASA | TN D-7635
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-7635 (Browse shelf) | Not for loan | TR12544 |
Total holds: 0
Boundary With Nasa Tn D-7631-34,7636-40.
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