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There are a total of 5 record(s) matching your query.
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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
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