Flight investigation of the effects of a partial span leading edge chord extension on the aerodynamic characteristics of a 35 deg swept wing fighter airplane frederick h van matteson isbn kostenloser versand fur alle bucher mit versand und verkauf duch amazon. Title flight investigation of the effects of a partial span leading edge chord extension on the aerodynamic characteristics of a 35 deg swept wing fighter airplane descriptive note research memo corporate author national aeronautics and space administration moffett field ca ames research center. Flight investigation of the effects of a partial span leading edge chord extension on the aerodynamic characteristics of a 35 deg swept wing fighter airplane descriptive note research memo corporate author national aeronautics and space administration moffett field ca ames research center personal authors matteson frederick h van dyke jr rudolph d report date 1954 04 23 . Flight investigation of the effects of a partial span leading edge chord extension on the aerodynamic characteristics of a 35 degree swept wing fighter airplane document id 19930088164 document type other authors van dyke rudolph d jr matteson frederick h date acquired august 16 2013 publication date april 23 1954 report patent number naca rm a54b26 distribution limits . Internet archive bookreader dtic ad0029198 flight investigation of the effects of a partial span leading edge chord extension on the aerodynamic characteristics of a 35 deg swept wing fighter airplane