Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
By: Stokes, Fred H.
Contributor(s): Matthews, J. T.
Material type: BookPublisher: Washington, D. C. National Advisory Committee for Aeronautics 1953Description: 41p.DDC classification: NACA | TN-2882Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | Reference | NACA TN-2882 (Browse shelf) | Not for loan | 67708B |
Total holds: 0
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