+ Visit NASA.gov + Contact NASA   + Home Select Search Field * All Report - Patent Number Abstract *Accession Number *NASA Center *Author NameDocument IDKeywordsPublication Date *Title * Find Results With All of the words At least one of the words Enter Search Term  within returned results    Search Tips: Use only the fields with * to search NIX collection. Enclose terms in double quotation marks (") to search for exact phrases, ie: "space shuttle". NOTE: Commas and dashes are removed from search term by search engine. Select Reset Search button to start a new search. See Help for more tips. + Publication Year + Subject + Item/Media Type Selected Navigations: Author > Bruckner, R. J. [x] Sort results by: NASA Center | Date Added to NTRS | Publication Year There are a total of 4 record(s) matching your query. Sorted by: Date Added To NTRS in Descending order Application of thin-film thermocouples to localized heat transfer measurements Author(s): Lepicovsky, J.; Bruckner, R. J.; Smith, F. A. Abstract: The paper describes a proof-of-concept experiment on thin-film thermocouples used for localized heat transfer measurements applicable to experiments on hot parts of turbine engines. The paper has three main parts. The first ... NASA Center: Glenn Research Center Publication Year: 1995 Added to NTRS: 2007-12-18 Accession Number: 96N13444; Document ID: 19960003435; Report Number: AIAA PAPER 95-2834, E-9890, NAS 1.15:107045, NASA-TM-107045, NIPS-95-05322 Modern Experimental Techniques in Turbine Engine Testing Author(s): Lepicovsky, J.; Bruckner, R. J.; Bencic, T. J.; Braunscheidel, E. P. Abstract: The paper describes application of two modern experimental techniques, thin-film thermocouples and pressure sensitive paint, to measurement in turbine engine components. A growing trend of using computational codes in ... NASA Center: Glenn Research Center Publication Year: 1996 Added to NTRS: 2005-08-25 Accession Number: 97N14973; Document ID: 19970009487; Report Number: E-10572, NAS 1.15:107383, NASA-TM-107383 Application of Pressure Sensitive Paint to Confined Flow at Mach Number 2.5 Author(s): Lepicovsky, J.; Bencic, T. J.; Bruckner, R. J. Abstract: Pressure sensitive paint (PSP) is a novel technology that is being used frequently in external aerodynamics. For internal flows in narrow channels, and applications at elevated nonuniform temperatures, however, there are ... NASA Center: Glenn Research Center Publication Year: 1998 Added to NTRS: 2005-08-25 Document ID: 19980197323; Report Number: AIAA Paper 97-3214, E-10842, NAS 1.15:107527, NASA/TM-1998-107527 Seeding for laser velocimetry in confined supersonic flows with shocks Author(s): Lepicovsky, J.; Bruckner, R. J. Abstract: There is a lack of firm conclusions or recommendations in the open literature to guide laser velocimeter (LV) users in minimizing the uncertainty of LV data acquired in confined supersonic flows with steep velocity ... NASA Center: Glenn Research Center Publication Year: 1996 Added to NTRS: 2005-08-25 Accession Number: 96N33972; Document ID: 19960049684; Report Number: E-10330, NAS 1.15:107265, NASA-TM-107265 + Back to Top + Sponsored by the NASA Scientific and Technical    Information Program + 2004 Vision for Space Exploration + Freedom of Information Act + NASA Web Privacy Policy and Important Notices + NASA Disclaimers, Copyright Notice,    and Terms and Conditions of Use NASA Official: Calvin Mackey Page Curator: NASA Center for AeroSpace Information (help@sti.nasa.gov) Last Updated: July 5, 2007