Design requirements of Bell X-22A, designed to explore mechanical and aerodynamic characteristics of dual-tandem, ducted-propeller V/STOL concept and to assess its military potential; description and general arrangement of aircraft, performance and control; variable stability and control system; handling characteristics in hover and transition; stall investigations and leading data.
Bell X-22A
Flight
Flight International ; 91 , n 3028
1967
5 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.