Model studies of crosswind landing-gear configurations for STOL aircraft
NASA (NTRS) · 1973
Overview
A dynamic model was used to directly compare four different crosswind landing gear mechanisms. The model was landed as a free body onto a laterally sloping runway used to simulate a crosswind side force. A radio control system was used for steering to oppose the side force as the model rolled to a…
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 ·
- 1973
- File size ·
- 1.5 MB