PERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL.
By: Niedzwiecki,Richard W.
Contributor(s): Moyer,Harry M.
Material type: BookPublisher: Nasa, Washington, D.C. 1969Description: 38.DDC classification: NASA | TN D-5597Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-5597 (Browse shelf) | Not for loan | TR12671 |
Total holds: 0
Bound With Nasa Tn D-5590-96, 5598-99 Lack No.5594
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