Wind-Tunnel Investigation at Low Speed of Effect of Size and Position of Closed Air Ducts on Static Longitudinal and Static Lateral Stability Characteristics of Unswept-Midwing Models Having Wings of Aspect Ratio 2, 4, and 6.
Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6
NACA -- Tech Note
1955
45 pages
Aufsatz (Zeitschrift)
Englisch
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