A THEORETICAL ANALYSIS OF A SIMPLE AERODYNAMIC DEVICE TO IMPROVE THE LONGITUDINAL DAMPING OF A CRUIFORM MISSILE CONFIGURATION AT SUPERSONIC SPEEDS
By: Clements,James B.
Material type: BookPublisher: 1957Description: 36.DDC classification: NACA | RM-L55H31Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | General Stacks | NACA RM-L55H31 (Browse shelf) | Not for loan | TR3501 |
Total holds: 0
Bound With Naca Rm L53a07
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