+ 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 + Subject + Availability Options + Item/Media Type Selected Navigations: Author > Spaid, F. W. [x] Sort results by: NASA Center | Date Added to NTRS | Publication Year There are a total of 15 record(s) matching your query. Sorted by: Date Added To NTRS in Descending order 1 2 Next  An experimental study of transonic flow about a supercritical airfoil. Static pressure and drag data obtained from tests of a supercritical airfoil and an NACA 0012 airfoil at transonic speeds, supplement Author(s): Spaid, F. W.; Dahlin, J. A.; Roos, F. W.; Stivers, L. S., Jr. Abstract: Surface static-pressure and drag data obtained from tests of two slightly modified versions of the original NASA Whitcomb airfoil and a model of the NACA 0012 airfoil section are presented. Data for the supercritical airfoil ... NASA Center: Ames Research Center Publication Year: 1983 Added to NTRS: 2008-07-31 Accession Number: 83N33846; Document ID: 19830025575; Report Number: A-8762, NAS 1.15:81336-SUPPL, NASA-TM-81336-SUPPL An experimental study of transonic flow about a supercritical airfoil Author(s): Spaid, F. W.; Dahlin, J. A.; Bachalo, W. D.; Stivers, L. S., Jr. Abstract: A series of experiments was conducted on flow fields about two airfoil models whose sections are slight modifications of the original Whitcomb supercritical airfoil section. Data obtained include surface static-pressure ... NASA Center: Ames Research Center Publication Year: 1983 Added to NTRS: 2008-07-31 Accession Number: 83N33845; Document ID: 19830025574; Report Number: A-8762, NAS 1.15:81336, NASA-TM-81336 Solid propellant combustion instability: Experiments with star grains Author(s): Landsbaum, E. M.; Spaid, F. W. Abstract: No Abstract Available NASA Center: Jet Propulsion Laboratory Publication Year: 1961 Added to NTRS: 2008-07-02 Accession Number: 74N70783; Document ID: 19740072844; Report Number: JPL-TR-32-227, NASA-CR-136575 Instrumentation for research on combustion instability in solid-propellant rocket motors Author(s): Landsbaum, E. M.; Spaid, F. W. Abstract: No Abstract Available NASA Center: Jet Propulsion Laboratory Publication Year: 1960 Added to NTRS: 2006-11-06 Accession Number: 65N82311; Document ID: 19650069910; Report Number: JPL-TR-34-42, NASA-CR-60986 Experimental studies of unstable combustion in solid-propellant rocket motors Author(s): Landsbaum, E. M.; Spaid, F. W. Abstract: No Abstract Available NASA Center: Jet Propulsion Laboratory Publication Year: 1961 Added to NTRS: 2006-11-06 Accession Number: 65N82419; Document ID: 19650070018; Report Number: JPL-TR-32-146, NASA-CR-57092 Secondary injection of gases into a supersonic flow Author(s): Spaid, F. W.; Zukoski, E. E. Abstract: Secondary injection of gases into supersonic flow NASA Center: NASA (non Center Specific) Publication Year: 1963 Added to NTRS: 2006-11-06 Accession Number: 64N19614; Document ID: 19640009700; Report Number: NASA-CR-53817 A study of secondary injection of gases into a supersonic flow Author(s): Rosen, R.; Spaid, F. W.; Zukoski, E. E. Abstract: Secondary injection of gases into supersonic flow NASA Center: Jet Propulsion Laboratory Publication Year: 1966 Added to NTRS: 2006-11-06 Accession Number: 66N32724; Document ID: 19660023434; Report Number: JPL-TR-32-834, NASA-CR-76891 EXPERIMENTS ON THE INTERACTION OF SECONDARY INJECTANTS AND ROCKET EXHAUST FOR THRUST VECTOR CONTROL Author(s): Newton, J. W., Jr.; Spaid, F. W. Abstract: Interaction of secondary fluids and rocket exhaust for thrust vector control NASA Center: Jet Propulsion Laboratory Publication Year: 1962 Added to NTRS: 2006-11-06 Accession Number: 62N10349; Document ID: 19620000349; Report Number: JPL-TR-32-203 Detailed transonic flow field measurements about a supercritical airfoil section Author(s): Hurley, F. X.; Spaid, F. W.; Roos, F. W.; Stivers, L. S., Jr.; Bandettini, A. Abstract: The transonic flow field about a Whitcomb-type supercritical airfoil profile was measured in detail. In addition to the usual surface pressure distributions and wake surveys, schlieren photographs were taken and velocity ... NASA Center: Ames Research Center Publication Year: 1975 Added to NTRS: 2004-11-03 Accession Number: 75N26975; Document ID: 19750018903; Report Number: A-5869, NASA-TM-X-3244 Measurements of the boundary layer and near wake of a supercritical airfoil at cruise conditions Author(s): Johnson, D. A.; Spaid, F. W. Abstract: The flow behavior within the upper-surface boundary layer and near wake of a supercritical airfoil operating at cruise conditions is discussed. Experimental results obtained from wind-tunnel tests are presented which provide ... NASA Center: Ames Research Center Publication Year: 1981 Added to NTRS: 2004-11-03 Accession Number: 81A45890; Document ID: 19810061486; Report Number: AIAA PAPER 81-1242 1 2 Next  + 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