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  Partner: UNT Libraries Government Documents Department
 Collection: National Advisory Committee for Aeronautics Collection
Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip

Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip

Date: April 7, 1955
Creator: Blackaby, James R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of a wing swept-back 63 degrees and twisted and cambered for a uniform load at a lift coefficient of 0.5

Wind-tunnel investigation at low speed of a wing swept-back 63 degrees and twisted and cambered for a uniform load at a lift coefficient of 0.5

Date: May 9, 1950
Creator: Weiberg, James A & Carel, Hubert C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of a wing swept back 63 degrees and twisted and cambered for uniform load at a lift coefficient of 0.5 and with a thickened tip section

Wind-tunnel investigation at low speed of a wing swept back 63 degrees and twisted and cambered for uniform load at a lift coefficient of 0.5 and with a thickened tip section

Date: November 21, 1950
Creator: Weiberg, James A & Carel, Hubert C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind Tunnel Investigation at Low Speed of Aerodynamic Characteristics of Army Chemical Corps Model E-112 Bomblets with Span Chord Ratio of 2 - 1

Wind Tunnel Investigation at Low Speed of Aerodynamic Characteristics of Army Chemical Corps Model E-112 Bomblets with Span Chord Ratio of 2 - 1

Date: December 26, 1956
Creator: Letko, W.
Description: An experimental investigation has been made in the Langley stability tunnel to determine the aerodynamic characteristics of the Army Chemical Corps model E-112 bomblets with span-chord ratio of 2:1. A detailed analysis has not been made; however, the results showed that all the models were spirally unstable and that a large gap between the model tips and end plates tended to reduce the instability.
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3.13 equipped with various 25-percent-chord plain flaps

Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3.13 equipped with various 25-percent-chord plain flaps

Date: April 1, 1950
Creator: Johnson, Harold S & Hagerman, John R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6

Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6

Date: September 1, 1955
Creator: Jaquet, Byron M & Williams, James L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of effects of sideslip on static longitudinal trim and static lateral stability characteristics of three fighter-type airplane models

Wind-tunnel investigation at low speed of effects of sideslip on static longitudinal trim and static lateral stability characteristics of three fighter-type airplane models

Date: September 11, 1956
Creator: Jaquet, Byron M & Fletcher, H S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of sideslipping, rolling, yawing, and pitching characteristics for a model of a 45 degree swept-wing fighter-type airplane

Wind-tunnel investigation at low speed of sideslipping, rolling, yawing, and pitching characteristics for a model of a 45 degree swept-wing fighter-type airplane

Date: September 1, 1955
Creator: Jaquet, Byron M & Fletcher, H S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of static and yawing characteristics of a 0.085-scale model of the Chance Vought XF8U-1 airplane : TED No. NACA DE 392

Wind-tunnel investigation at low speed of static and yawing characteristics of a 0.085-scale model of the Chance Vought XF8U-1 airplane : TED No. NACA DE 392

Date: January 19, 1954
Creator: Jaquet, Byron M & Williams, James L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of the aerodynamic characteristics of the Army Chemical Corps model E112 bomblets

Wind-tunnel investigation at low speed of the aerodynamic characteristics of the Army Chemical Corps model E112 bomblets

Date: November 4, 1955
Creator: Letko, William & Williams, James L
Description: None
Contributing Partner: UNT Libraries Government Documents Department