Aerodynamic stability and control of ducted- propeller aircraft
· NASA (NTRS) · 1966
Public domain · NASA (NTRS)Technical Reports
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…
- Publisher
- NASA (NTRS)
- Document
- Year
- 1966
Source & rights
Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.
Permanent URL — we don’t break links.
Document details
- Doc number
- Publisher
- NASA (NTRS)
- Year
- 1966
- File size
- 1.0 MB