+ 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 + Availability Options + Item/Media Type Selected Navigations: Author > Inger, G. R. [x] Sort results by: NASA Center | Date Added to NTRS | Publication Year There are a total of 5 record(s) matching your query. Sorted by: Date Added To NTRS in Descending order Turbulent eddy viscosity modeling in transonic shock/boundary-layer interactions Author(s): Inger, G. R. Abstract: The treatment of turbulence effects on transonic shock/turbulent boundary layer interaction is addressed within the context of a triple deck approach valid for arbitrary practical Reynolds numbers between 1000 and 10 ... NASA Center: NASA (non Center Specific) Publication Year: 1989 Added to NTRS: 2008-05-30 Accession Number: 89N20952; Document ID: 19890011581 Asymptotic analytical methods in fluid mechanics related to drag prediction Author(s): Inger, G. R. Abstract: Some recent theoretical work of a purely analytical nature is described which promises to provide engineering predictions for the important drag-related phenomena of flow in the stall regime. This analytical work deals with ... NASA Center: NASA (non Center Specific) Publication Year: 1975 Added to NTRS: 2004-11-03 Accession Number: 76N11006; Document ID: 19760003918 Analytical study of subsonic turbulent boundary layer separation including viscous-inviscid interaction Author(s): Inger, G. R. Abstract: The prediction of boundary layer deceleration and separation in regions of adverse pressure gradients are discussed as an unsolved problem of fundamental practical importance in aerodynamics. A three layered theoretical flow ... NASA Center: NASA (non Center Specific) Publication Year: 1974 Added to NTRS: 2004-11-03 Accession Number: 75N12254; Document ID: 19750004182; Report Number: NASA-CR-140958, VPI-AERO-026 Application of unsteady laminar triple-deck theory to viscous-inviscid interactions from an oscillating flap in supersonic and subsonic flow Author(s): Inger, G. R.; Huang, M.-K. Abstract: Unsteady triple-deck theory is applied to analyze the local viscous-inviscid interaction of an idealized oscillating flap with a laminar boundary layer in either supersonic or subsonic external flow. For small flap ... NASA Center: NASA (non Center Specific) Publication Year: 1983 Added to NTRS: 2004-11-03 Accession Number: 83A44457; Document ID: 19830063239 Supersonic laminar base pressure, heat-transfer, and upstream influence correlations for small steps Author(s): Inger, G. R. Abstract: Some results of the application of a unified theory of small disturbances in nonuniform high-speed boundary layers to the small-step problem for the case of supersonic laminar nonadiabatic flow are described. Comparisons ... NASA Center: NASA (non Center Specific) Publication Year: 1974 Added to NTRS: 2004-11-03 Accession Number: 74A38628; Document ID: 19740055878 + 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