+ 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. + NASA Center + Publication Year + Item/Media Type Selected Navigations: Author > Carman, L Robert [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 Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid Author(s): Carman, L Robert Abstract: No Abstract Available NASA Center: Glenn Research Center Publication Year: 1945 Added to NTRS: 2006-11-06 Accession Number: 93R22391; Document ID: 19930093101; Report Number: NACA-ACR-E5C30, NACA-WR-E-216 The effect of inlet temperature and pressure on the efficiency of single-stage impulse turbine having a 13.2-inch pitch-line diameter wheel Author(s): Carman, L Robert Abstract: No Abstract Available NASA Center: Glenn Research Center Publication Year: 1945 Added to NTRS: 2006-11-06 Accession Number: 93R22387; Document ID: 19930093097; Report Number: NACA-ARR-E5H10, NACA-WR-E-232 The performance of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with cast airfoil-shaped and bent sheet-metal nozzle blades Author(s): Carman, L Robert Abstract: No Abstract Available NASA Center: Glenn Research Center Publication Year: 1945 Added to NTRS: 2006-11-06 Accession Number: 93R22389; Document ID: 19930093099; Report Number: NACA-ARR-E5H31, NACA-WR-E-233 Lift and drag coefficients for the Bell X-1 airplane (8-percent-thick wing) in power-off transonic flight Author(s): Carman, L Robert; Carden, John R Abstract: No Abstract Available NASA Center: Langley Research Center Publication Year: 1951 Added to NTRS: 2006-11-06 Accession Number: 93R15986; Document ID: 19930086696; Report Number: NACA-RM-L51E08 + 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