1977-02-01

The Controlwing Aircraft 770474

ABSTRACT

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.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 43% off list price.
Login to see discount.
Special Offer: With TechSelect, you decide what SAE Technical Papers you need, when you need them, and how much you want to pay.
X