EFFECTS OF ANGLE OF ATTACK AND THICKNESS RATIO ON THE FLUTTER OF RIGID UNSWEPT DIAMOND-AIRFOIL-SECTION WING AT A MACH NUMBER OF 10.0
By: Young,Lou S.
Material type:
BookPublisher: Nasa, Washington, D.C. 1962Description: 23.DDC classification: NASA | TN D-1380
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-1380 (Browse shelf) | Not for loan | TR12901 |
Total holds: 0
Bound With Nasa Tn D-1376-79
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