Abstract: An efficient aircraft utilizes a stabilizer spaced from a fixed wing, and supported for controlled rolling about an axis extending generally in a forward direction, to control aircraft yaw. The stabilizer extends generally horizontally in straight forward flight. Pitch of the stabilizer is also controlled.
Type:
Grant
Filed:
July 24, 1978
Date of Patent:
June 10, 1980
Assignee:
Paul B. MacCready, Jr.
Inventors:
Paul B. MacCready, Jr., Peter B. S. Lissaman, James D. Burke