Publication Date:
2019-08-15
Description:
An investigation has been made in the Langley free-flight tunnel to determine the low-speed static lateral stability characteristics and the rolling, yawing, and sideslipping dynamic stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane. The results of this investigation are presented herein without analysis.
Keywords:
Aircraft Stability and Control
Type:
NASA-TN-D-433
,
L-640
Format:
application/pdf