Aerodynamic stability and control of ducted- propeller aircraft
NASA (NTRS) · 1966
Overview
Test results from studies of small and large powered models of a dual, tandem, ducted-propeller VTOL design are reviewed, with emphasis on stability and control characteristics through the transition speed range. The characteristics are generally satisfactory. Stability augmentation may be…
Source & rights
Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.
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Document details
- Doc number ·
- Publisher ·
- NASA (NTRS)
- Year ·
- 1966
- File size ·
- 1.0 MB