Investigation was made for three different wing positions and two horizontal tail positions for each wing position and included measurements of both longitudinal and lateral stability characteristics.
Wind-tunnel investigation of aerodynamic characteristics of model representative of supersonic fighter-class airplane with external-flow jet-augmented flap in low-speed flight
NASA -- Tech Note
1959
84 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.