Abstract: A jet thrust aircraft wing wherein the intake and exhaust are substantially coextensive with the leading and trailing edges, respectively; utilizing engine suction to induce intake of air and preventing build-up ahead of the wing by separating the same from the flow of air over and under the upper and lower wing surfaces; and utilizing engine exhaust thrust to induce controllable air flow through the wing and to induce longitudinal flow of air over and under the wing throughout its span.
Type:
Grant
Filed:
June 5, 1975
Date of Patent:
May 31, 1977
Assignees:
Mark S. Grow, Bonnie B. Madden, Michael J. Grow