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The Controlwing Aircraft
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1977 by SAE International in United States
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A new concept in aircraft control and stability has been developed having greater control effectiveness than the Aileron, rudder, elevator system. It is structurally simple having no movable vanes subject to flutter. There are no stall or spin characteristics. This system has natural gust-alleviation properties and as there are but two primary controls no coordination is needed in piloting.
|Technical Paper||Devices for Improvement of Controllability at Stall|
|Technical Paper||Aerodynamic Design Approach to the Stall/Spin Problem - The VariViggen|
|Technical Paper||STALL/SPIN STUDIES RELATING TO LIGHT GENERAL-AVIATION AIRCRAFT|