Carl J Wenzinger

发表

Pressure Distribution Over Airfoils With Fowler Flaps

Carl J Wenzinger, Walter B Anderson, 1938 .

Rolling Moments Due to Rolling and Yaw for Four Wing Models in Rotation

Montgomery Knight, Carl J Wenzinger, 1932 .

Wind tunnel pressure distribution tests on an airfoil with trailing edge flap

Oscar Loeser, Carl J Wenzinger, 1929 .

Wind-Tunnel Investigation of an N.A.C.A. 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flap

Carl J Wenzinger, Willikam E Gauvain, C. J. Wenzinger, 1938 .

Pressure distribution over an NACA 23012 airfoil with a slotted and a plain flap

Carl J Wenzinger, James B Delano, 1938 .

Resume of air-load data on slats and flaps

Carl J Wenzinger, Francis M Rogallo, 1939 .

Wind-Tunnel Investigation of Spoiler, Deflector, and Slot Lateral-Control Devices on Wings With Full-Span Split and Slotted Flaps

Carl J Wenzinger, Francis M Rogallo, 1941 .

Pressure distribution over a Clark Y-H airfoil section with a split flap

Carl J Wenzinger, 1937 .

Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps

Carl J Wenzinger, 1937 .

Wind-tunnel tests of a Clark Y wing having split flaps with gaps

Carl J Wenzinger, 1938 .

Wind-tunnel investigation of the aerodynamic balancing of upper-surface ailerons and split flaps

Carl J Wenzinger, 1937 .

Pressure distribution over an NACA 23012 airfoil with an NACA 23012 external-airfoil flap

Carl J Wenzinger, 1938 .

Wind-tunnel measurements of air loads on split flaps

Carl J Wenzinger, 1934 .