THEORY FOR COMPUTING SPAN LOADS AND STABILITY DERIVATIVES DUE TO SIDESLIP YAWING AND ROLLING FOR WINGS IN SUBSONIC COMPRESSIBLE FLOW
By: Queijo,M J.
Material type:
BookPublisher: Nasa, Washington, D.C. 1968Description: 76.DDC classification: NASA | TN D-4929
| 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-4929 (Browse shelf) | Not for loan | TR12449 |
Total holds: 0
Bound With Nasa Tn D-4921-28, 4930.
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