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[Herman Lurie's Weekly Report, December 4, 1953] (open access)

[Herman Lurie's Weekly Report, December 4, 1953]

Weekly report discussing the state of the raw sugar market, including details for prices and market fluctuations related to weights in tons, regions, distribution, years, and figures.
Date: December 4, 1953
Creator: Lurie, Herman
System: The Portal to Texas History
[Imperial Sugar Company Estimated Daily Cash Balances: December 4, 1953] (open access)

[Imperial Sugar Company Estimated Daily Cash Balances: December 4, 1953]

Daily cash report for Imperial Sugar Company including a list of large withdrawls for the months surrounding the date showing the daily expenses and estimated balance for each entry. It also lists scheduled payments for bank loans.
Date: December 4, 1953
Creator: Imperial Sugar Company
System: The Portal to Texas History
Investigation of a High-Pressure-Ratio Eight-Stage Axial-Flow Research Compressor With Two Transonic Inlet Stages 1: Aerodynamic Design (open access)

Investigation of a High-Pressure-Ratio Eight-Stage Axial-Flow Research Compressor With Two Transonic Inlet Stages 1: Aerodynamic Design

Memorandum presenting an eight-stage high-pressure-ratio axial-flow compressor designed for use as a research unit in which the problems associated with design and off-design performance of transonic stages combined with highly loaded subsonic stages could be studied. The report discusses the design procedure and presents the experimentally determined overall performance of the compressor.
Date: December 4, 1953
Creator: Voit, Charles H.
System: The UNT Digital Library
Wind-Tunnel Investigation at High and Low Subsonic Mach Numbers of Two Unswept Wings Having NACA 2-006 and NACA 65A006 Airfoil Sections (open access)

Wind-Tunnel Investigation at High and Low Subsonic Mach Numbers of Two Unswept Wings Having NACA 2-006 and NACA 65A006 Airfoil Sections

Report presenting an investigation in the low-turbulence pressure tunnel to determine the lift, drag, and pitching-moment characteristics of two unswept wings, one with airfoil sections designed for high maximum lift at low speeds (NACA 2-006) and one with NACA 65A006 airfoil sections. Results regarding lift and pitching-moment, effects of roughness, drag, and wings with flaps are provided for high- and low-speed performance.
Date: December 4, 1953
Creator: Racisz, Stanley F.
System: The UNT Digital Library
Experimental Determination of Gas Motion Accompanying Screeching Combustion in a 6-Inch Simulated Afterburner (open access)

Experimental Determination of Gas Motion Accompanying Screeching Combustion in a 6-Inch Simulated Afterburner

Report presenting an investigation to develop screech instrumentation and study the mechanism of screech in a simulated afterburner. Results regarding the screech mechanism, effect of system variables on screech, speculation regarding screech mechanism, and suggested techniques for elimination or control of screech are provided.
Date: December 4, 1953
Creator: Blackshear, Perry L.; Rayle, Warren D. & Tower, Leonard K.
System: The UNT Digital Library
Analysis of part-speed operation for high-pressure-ratio multistage axial-flow compressors (open access)

Analysis of part-speed operation for high-pressure-ratio multistage axial-flow compressors

From Introduction: "For the analysis reported herein, the same hypothetical 12-stage compressor discussed in reference 6 was chosen, and the effects of inlet-stage stall characteristics and stage interactions were estimated by arbitrary adjustment of the stall characteristics and stage interactions were estimated by arbitrary adjustment of the stalled characteristics of the individual stages."
Date: December 4, 1953
Creator: Benser, William A.
System: The UNT Digital Library
Experimental investigation of screeching combustion in full-scale afterburner (open access)

Experimental investigation of screeching combustion in full-scale afterburner

Report presenting an investigation using a number of systematic configuration modifications to an afterburner to determine their effect on screech characteristics. The modifications included changes in the afterburner diffuser, the fuel system, and the flame holder. Results regarding some of the characteristics of screeching combustion, effect of diffuser flow conditions, and effect of fuel system and flame holder are provided.
Date: December 4, 1953
Creator: Usow, Karl H.; Meyer, Carl L. & Schulze, Frederick W.
System: The UNT Digital Library