AbstractAn attempt is made to construct a data-acquisition system to measure the in-flight loads of an autogyro. These results give an indication of the scale of pilot forces and of those acting in the control linkage of the rotor.Keywordsautogyrorotordata acquisition systemin-flight loadsGet full access to this articleView all access options for this article.Get accessReferences1.AAIB Bulletin 4/95, Air Accidents Investigation Branch, DRA, Farnborough, Hampshire.
