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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1957
 Month: September
 Collection: Technical Report Archive and Image Library
Aerodynamic performance of several techniques for spike-position control of  a blunt-lip nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to 2.0

Aerodynamic performance of several techniques for spike-position control of a blunt-lip nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to 2.0

Date: September 17, 1957
Creator: Anderson, Arthur A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Altitude Starting Tests of a 1000-Pound-Thrust Solid-Propellant Rocket

Altitude Starting Tests of a 1000-Pound-Thrust Solid-Propellant Rocket

Date: September 13, 1957
Creator: Sloop, John L.
Description: Four solid-propellant rocket engines of nominal 1000-pound-thrust were tested for starting characteristics at pressure altitudes ranging from 112,500 to 123,000 feet and at a temperature of -75 F. All engines ignited and operated successfully. Average chamber pressures ranged from 1060 to ll90 pounds per square inch absolute with action times from 1.51 to 1.64 seconds and ignition delays from 0.070 t o approximately 0.088 second. The chamber pressures and action times were near the specifications, but the ignition delay was almost twice the specified value of 0.040 second.
Contributing Partner: UNT Libraries Government Documents Department
Analysis of shock motion in ducts during disturbances in downstream pressure

Analysis of shock motion in ducts during disturbances in downstream pressure

Date: September 1, 1957
Creator: Hurrell, Herbert G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of obliquely mounted strain gage to measurement of residual stresses in disks

Application of obliquely mounted strain gage to measurement of residual stresses in disks

Date: September 1, 1957
Creator: Hirschberg, M H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine

Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine

Date: September 1, 1957
Creator: Lassiter, Leslie W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Chemical Processing Instrumentation and Control Research Program

Chemical Processing Instrumentation and Control Research Program

Date: September 18, 1957
Creator: Schneider, Harry
Description: Report regarding the chemical processing instrumentation designs and problems at the Idaho Chemical Processing Plant.
Contributing Partner: UNT Libraries Government Documents Department
Comparison of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models having externally braced wings and cantilever wings

Comparison of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models having externally braced wings and cantilever wings

Date: September 25, 1957
Creator: Dickens, Waldo L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Compressibility effects on a hovering helicopter rotor having an NACA 0018 root airfoil tapering to an NACA 0012 tip airfoil

Compressibility effects on a hovering helicopter rotor having an NACA 0018 root airfoil tapering to an NACA 0012 tip airfoil

Date: September 25, 1957
Creator: Powell, Robert D , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Determination of surge and stall limits of an axial-flow turbojet engine for control applications

Determination of surge and stall limits of an axial-flow turbojet engine for control applications

Date: September 1, 1957
Creator: Schmidt, Ross D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of conical and flat sting-mounted windshields on the zero-lift drag of a flare-stabilized bluff body at Mach numbers from 0.6 to 1.15

Effect of conical and flat sting-mounted windshields on the zero-lift drag of a flare-stabilized bluff body at Mach numbers from 0.6 to 1.15

Date: September 12, 1957
Creator: Blanchard, Willard S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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