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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1957
 Collection: Technical Report Archive and Image Library
Transonic flutter investigation of a cantilevered, aspect-ratio-4, 45 degree sweptback, untapered wing with three different pylon-mounted external store configurations

Transonic flutter investigation of a cantilevered, aspect-ratio-4, 45 degree sweptback, untapered wing with three different pylon-mounted external store configurations

Date: July 5, 1957
Creator: Ruhlin, Charle L & Bowwinkle, Robert W , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic Flutter Investigation of an All-movable Horizontal Tail for a Fighter Airplane

Transonic Flutter Investigation of an All-movable Horizontal Tail for a Fighter Airplane

Date: January 14, 1957
Creator: Abbott, F. T., Jr. & Land, N. S.
Description: Transonic flutter of all-movable horizontal tail - bending & pitching moments.
Contributing Partner: UNT Libraries Government Documents Department
Transonic flutter investigation of an all-moveable horizontal tail for a fighter airplane

Transonic flutter investigation of an all-moveable horizontal tail for a fighter airplane

Date: January 14, 1957
Creator: Land, Norman S & Abbott, Rank T , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic flutter investigation of arrowhead wing with tip ailerons and trailing-edge flaps

Transonic flutter investigation of arrowhead wing with tip ailerons and trailing-edge flaps

Date: November 4, 1957
Creator: Jones, George W & Boswinkle, Robert W , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic flutter investigation of two 64 degree delta wings with simulated streamwise rib and orthogonal spar construction

Transonic flutter investigation of two 64 degree delta wings with simulated streamwise rib and orthogonal spar construction

Date: January 4, 1957
Creator: Jones, George W , Jr & Young, Lou S , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic investigation of an axial-flow compressor rotor with a hub-tip ratio of 0.75 and blades having NACA A(sub 2)I(Sub 8b) mean lines

Transonic investigation of an axial-flow compressor rotor with a hub-tip ratio of 0.75 and blades having NACA A(sub 2)I(Sub 8b) mean lines

Date: September 30, 1957
Creator: Bernot, Peter T & Savage, Melvyn
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic investigation of effects of spanwise and chordwise external store location and body contouring on aerodynamic characteristics of 45 degree sweptback wing-body configuration

Transonic investigation of effects of spanwise and chordwise external store location and body contouring on aerodynamic characteristics of 45 degree sweptback wing-body configuration

Date: September 25, 1957
Creator: Pearson, Albin O
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic investigation of internal-flow characteristics of a square-shaped scoop inlet mounted at three chordwise positions above a high 45 degree sweptback wing and body combination

Transonic investigation of internal-flow characteristics of a square-shaped scoop inlet mounted at three chordwise positions above a high 45 degree sweptback wing and body combination

Date: April 17, 1957
Creator: Keith, Arvid L , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A transonic investigation of the mass-flow and pressure recovery characteristics of several types of auxiliary air inlets

A transonic investigation of the mass-flow and pressure recovery characteristics of several types of auxiliary air inlets

Date: April 10, 1957
Creator: Dennard, John S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic loads characteristics of a 3-percent-thick 60 degree delta-wing-body combination

Transonic loads characteristics of a 3-percent-thick 60 degree delta-wing-body combination

Date: May 28, 1957
Creator: Swihart, John M & Foss, Willard E , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department