Variations of total forces and moments with angles of attack and sideslip, calculated for number of slender plane and cruciform wing-tail combinations under assumption that vortex sheet is fully rolled up ahead of tail.
Aerodynamic interference of slender wing-tail combinations
NACA -- Tech Note
1957
81 pages
Report
English
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Aerodynamic forces on slender plane- and cruciform-wing and body combinations
Engineering Index Backfile | 1950
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