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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Collection: Technical Report Archive and Image Library
Wind-Tunnel Investigation of a 1/60-Scale Model of the Republic MX-1554 Airplane at a Mach Number of 2.85

Wind-Tunnel Investigation of a 1/60-Scale Model of the Republic MX-1554 Airplane at a Mach Number of 2.85

Date: March 18, 1953
Creator: Dickey, R. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a 45 degree sweptback wing having a symmetrical root and a highly cambered tip, including the effects of fences and lateral controls

Wind-tunnel investigation of a 45 degree sweptback wing having a symmetrical root and a highly cambered tip, including the effects of fences and lateral controls

Date: November 20, 1953
Creator: Cleary, Joseph W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel Investigation of a Full-Scale Model of the Hughes MX-904 Missile

Wind-Tunnel Investigation of a Full-Scale Model of the Hughes MX-904 Missile

Date: January 1, 1950
Creator: unknown
Description: A wind-tunnel investigation has been conducted to determine the stability and control characteristics of a full-size model of the Hughes MX-904 missile. Aerodynamic characteristics of the complete model through moderate ranges of angles of attack and yaw, with an additional test made through an angle of attack of 180 degrees, are presented. The effects of horizontal tail deflection are also included.
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel Investigation of a Modified 1/20-Scale Model of the Convair MX-1554 Airplane at Mach Numbers of 1.41 and 2.01

Wind-Tunnel Investigation of a Modified 1/20-Scale Model of the Convair MX-1554 Airplane at Mach Numbers of 1.41 and 2.01

Date: August 24, 1953
Creator: Hilton, John H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel Investigation of a Number of Total Pressure Tubes at High Angles of Attack

Wind-Tunnel Investigation of a Number of Total Pressure Tubes at High Angles of Attack

Date: January 1, 1951
Creator: Gracey, William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack : subsonic speeds

Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack : subsonic speeds

Date: April 1, 1951
Creator: Gracey, William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack -- subsonic, transonic, and supersonic speeds

Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack -- subsonic, transonic, and supersonic speeds

Date: January 1, 1957
Creator: Gracey, William
Description: The effect of inclination of the airstream on the measured pressures of 54 total-pressure tubes has been determined for angles of attack up to 60 degrees and over a Mach number range from 0.26 to 1.62. The investigation was conducted in five wind tunnels at the Langley Aeronautical Laboratory.
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack subsonic, transonic, and supersonic speeds

Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack subsonic, transonic, and supersonic speeds

Date: May 1, 1956
Creator: Gracey, William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a ram-jet canard missile model having a wing and canard surfaces of delta plan form with 70 degree swept leading edges : longitudinal and lateral stability and control characteristics at a Mach number of 1.60

Wind-tunnel investigation of a ram-jet canard missile model having a wing and canard surfaces of delta plan form with 70 degree swept leading edges : longitudinal and lateral stability and control characteristics at a Mach number of 1.60

Date: August 1, 1952
Creator: Spearman, M Leroy
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a ram-jet missile model having a wing and canard surfaces of delta plan form with 70 degrees swept leading edges : force and moment characteristics of various combinations of components at a Mach number of 1.6

Wind-tunnel investigation of a ram-jet missile model having a wing and canard surfaces of delta plan form with 70 degrees swept leading edges : force and moment characteristics of various combinations of components at a Mach number of 1.6

Date: March 9, 1953
Creator: Sevier, John R , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department