EFFECT OF REYNOLDS NUMBER ON THE LATERAL-STABILITY DERIVATIVES AT LOW SPEED OF SWEPTBACK- AND DELTA-WING-FUSELAGE COMBINATIONS OSCILLATING IN YAW
By: Llewellyn,Charles P.
Contributor(s): Wolhart,Walter D.
Material type:
BookPublisher: Nasa, Washington, D.C. 1960Description: 45.DDC classification: NASA | TN D-398
| 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-398 (Browse shelf) | Not for loan | TR15931 |
Total holds: 0
Bound With Nasa Tn D-391-97,399-400
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