Comparison of wind-tunnel and flight results on a four-propeller tilt-wing configuration
NASA (NTRS) · 1966
Overview
Over the years aerodynamicists have learned to rely heavily on wind-tunnel-model results in predicting the aerodynamic characteristics of conventional aircraft configurations. With the development of V/STOL configurations which have high slipstream deflection angles. such as the four-propeller…
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 ·
- 1.5 MB