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Over-all performance of J35-A-23 two-stage turbine

Description: Over-all performance of a two-stage turbine from a J35-A-23 turbojet engine is presented. Limiting blade loading restricted work output to approximately 95 percent of the design value. The brake internal efficiency at design operating conditions was approximately 0.75. maximum brake internal efficiency at off-design conditions was between 0.81 and 0.82.
Date: December 10, 1951
Creator: Rebeske, John J., Jr.; Berkey, William E. & Forrette, Robert E.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Report of the Thirty-Sixth National Conference on Weights and Measures, 1951

Description: Report of the annual conference on weights and measures, hosted by the U.S. National Bureau of Standards in Washington D.C. It includes conference proceedings, a list of attendees, information about committees and officers, and other reports or commentaries discussed at the meetings.
Date: December 10, 1951
Creator: United States. National Bureau of Standards.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Graphic Analysis of American and British Axial-Flow Turbojet Engine Performance Trends (Current and Future)

Description: From Summary: "This report presents a compilation of static sea-level data on existing or designed American and British axial-flow turbojet engines in terms of basic engine parameters such as thrust and air flow. In the data presented, changes in the over-U engine performance with time are examined as well as the relation of the various engine parameters to each other."
Date: December 10, 1951
Creator: Cesaro, Richard S. & Lazar, James
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
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