Study made in transonic Ames wind tunnel to investigate effectiveness of tail; lift, drag, and pitching moment coefficients are determined and effective downwash characteristics at tail evaluated and presented.
Effectiveness of all-movable horizontal tail on unswept-wing and body combination for mach numbers from 0.60 to 1.40
NASA -- Tech Note
1959
23 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.