Analytical investigation of the spin and recovery characteristics of a supersonic trainer airplane having a 24o swept wing [NASA TM X-606]
Material type:
- NASA TM X-606
Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
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PK Kelkar Library, IIT Kanpur | Reference | NASA TM X-606 (Browse shelf(Opens below)) | Not for loan | 102484 |
Total holds: 0
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