An investigation has been conducted in the Langley stability tunnel to determine the effect of an unswept wing on the contribution of unswept-tail configurations to the low-speed static and rolling-stability derivatives of a midwing airplane model.
Effect of an Unswept Wing on the Contribution of Unswept-Tail Configurations to the Low-Speed Static- and Rolling-Stability Derivatives of a Midwing Airplane Model
1950
46 pages
Report
Keine Angabe
Englisch
Engineering Index Backfile | 1956
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