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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Cavitation damage investigations in mixed-flow liquid metal pumps.
Cavitation damage in high-temperature liquid metal pumps for Rankine cycle space power plants studied in water model
Experimental studies of cavitation damage in alkali metal pumps for application in space power systems.
Cavitation damage in alkali metal pumps, noting damage resistance and material properties for application in space power systems
Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, part 2
Presented here are 59 abstracts and presentations and three invited presentations given at the Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion held at the George C. Marshall Space Flight Center, April 28-30, 1992. The purpose of the workshop is to discuss experimental and computational fluid dynamic activities in rocket propulsion. The workshop is an open meeting for government, industry, and academia. A broad number of topics are discussed, including a computational fluid dynamic methodology, liquid and solid rocket propulsion, turbomachinery, combustion, heat transfer, and grid generation.
Method of Designing Vaneless Diffusers and Experimental Investigation of Certain Undetermined Parameters
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Performance of a Double-row Radial Aircraft Engine with Three Methods of Safety-fuel Injection
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Apparent Effect of Inlet Temperature on Adiabatic Efficiency of Centrifugal Compressors
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Experimental Study of Effect of Vaneless-diffuser Diameter on Diffuser Performance
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Determination of centrifugal-compressor performance on basis of static-pressure measurements in vaneless diffuser
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Two-dimensional compressible flow in centrifugal compressors with straight blades
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Two-dimensional compressible flow in centrifugal compressors with logarithmic-spiral blades
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Analysis of cooling limitations and effect of engine-cooling improvements on level-flight cruising performance of a four-engine heavy bomber
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User’s Guide for the NASA High Efficiency Centrifugal Compressor Data Archive
The datasets contained in this archive are associated with the High Efficiency Centrifugal Compressor (HECC) in the Small Engine Components Compressor Test Facility, colloquially referred to as CE-18, at NASA Glenn Research Center. The archive is accessible at https://storage.googleapis.com/hecc-data/NASA-HECC-Data-Archive.zip. The documentation contained herein provides context for the data hosted on data.nasa.gov. The datasets and accompanying content in this document will be updated periodically as additional data is procured analyzed. The revision of the document is provided by date in the footer, and the revision updates are provided in the Revisions section. Please contact Trey Harrison (email: herbert.harrison@nasa.gov) for inquiries related to the dataset and documentation or to be added to an email list to be notified of updates and additions to the archive.
Queen City Forging Revitalized by Oak Ridge National Lab Partnership – U.S. Department of Energy
Oak Ridge National Laboratory, with support from the U.S. Department of Energy, teamed up with Queen City Forging, the U.S. Forging Industry, and Infrared Heating Technologies to develop a rapid-infrared heating furnace to produce aluminum turbochargers.