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  Partner: UNT Libraries Government Documents Department
 Decade: 1940-1949
Wind-tunnel investigation of horizontal tails I : unswept and 35 degrees swept-back plan forms of aspect ratio 3

Wind-tunnel investigation of horizontal tails I : unswept and 35 degrees swept-back plan forms of aspect ratio 3

Date: April 22, 1948
Creator: Dods, Jules B , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of horizontal tails II : unswept and 35 degree swept-back plan forms of aspect ratio 4.5

Wind-tunnel investigation of horizontal tails II : unswept and 35 degree swept-back plan forms of aspect ratio 4.5

Date: June 3, 1948
Creator: Dods, Jules B , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of horizontal tails III : unswept and 35 degrees swept-back plan forms of aspect ratio 6

Wind-tunnel investigation of horizontal tails III : unswept and 35 degrees swept-back plan forms of aspect ratio 6

Date: December 17, 1948
Creator: Dods, Jules, B , jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of horizontal tails IV : unswept plan form of aspect ratio 2 and a two-dimensional model

Wind-tunnel investigation of horizontal tails IV : unswept plan form of aspect ratio 2 and a two-dimensional model

Date: December 16, 1948
Creator: Dods, Jules B , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of horizontal tails V : 45 degree swept-back plan form of aspect ratio 2

Wind-tunnel investigation of horizontal tails V : 45 degree swept-back plan form of aspect ratio 2

Date: September 27, 1949
Creator: Dods, Jules B JR
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of icing of an engine cooling-fan installation

Wind-tunnel investigation of icing of an engine cooling-fan installation

Date: April 1, 1947
Creator: Lewis, J. P.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of icing of an engine cooling-fan installation

Wind-tunnel investigation of icing of an engine cooling-fan installation

Date: April 1, 1947
Creator: Lewis, James P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel investigation of NACA 65,3-418 airfoil section with boundary-layer control through a single suction slot applied to a plain flap

Wind-Tunnel investigation of NACA 65,3-418 airfoil section with boundary-layer control through a single suction slot applied to a plain flap

Date: February 23, 1949
Creator: Horton, Elmer A & Von Doenhoff, Albert E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind tunnel investigation of NACA 66(215)-216, 66,1-212, and 65(sub 1)-212 airfoils with 0.20-airfoil-chord split flaps

Wind tunnel investigation of NACA 66(215)-216, 66,1-212, and 65(sub 1)-212 airfoils with 0.20-airfoil-chord split flaps

Date: July 1, 1944
Creator: Fullmer, Felicien F , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double slotted flaps

Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double slotted flaps

Date: January 1, 1941
Creator: Harris, Thomas A & Recant, Isidore G
Description: Report presents the results of an investigation conducted in the NACA 7 by 10-foot win tunnel to determine the effect of the deflection of main and auxiliary slotted flaps on the aerodynamic section characteristics of large-chord NACA 23012, 23021, 23030 airfoils equipped with 40-percent-chord double slotted flaps. The complete aerodynamic section characteristics and envelope polar curves are given for each airfoil-flap combination. The effect of airfoil thickness is shown, and comparisons are made of single slotted flaps with double slotted flaps on each of the airfoils.
Contributing Partner: UNT Libraries Government Documents Department