Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
7 results returnedSearch results
- Wind-tunnel investigation of the effect of tab balance on tab and control-surface characteristics
- Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps
- Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50- airfoil chord plain sealed flaps
- Effect of Taper Ratio on the Low-Speed Rolling Stability Derivatives of Swept and Unswept Wings of Aspect Ratio 2.61
- Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces
- Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61
- Description and bibliography of NACA research on wing controls: January 1946 - February 1955