LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION HAVING SPLIT FLAPS LOCATED AHEAD OF THE WING TRAILING EDGE AND LEADING-AND TRAILING -EDGE FLAPS ON THE CANARD CONTROL
By: Spencer,Bernard.
Material type: BookPublisher: Nasa, Washington, D.C. 1962Description: 54.DDC classification: NASA | TN D-1245Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-1245 (Browse shelf) | Not for loan | TR12804 |
Total holds: 0
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Bound With Nasa Tn D-1241-44, 1246-50
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