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There are a total of 15 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Experimental Investigation of Boundary Layer Behavior in a Simulated Low Pressure Turbine
Author(s): Shyne, Rickey J.; Sohn, Ki-Hyeon; DeWitt, Kenneth J.
Abstract: A detailed investigation of the flow physics occurring on the suction side of a simulated Low Pressure Turbine (LPT) blade was performed. A contoured upper wall was designed to simulate the y pressure distribution of an ...
NASA Center: Glenn Research Center
Publication Year: 1999
Added to NTRS: 2008-06-02
Document ID: 20000067663
Overview of NASP nozzle research
Author(s): Trefny, Charles J.; Shyne, Rickey J.; Carboni, Jeanne D.
Abstract: Problems facing the National Aerospace Plane (NASP) nozzle at transonic and low supersonic conditions are discussed. An overview of NASP nozzle research at Lewis Research Center is given. Experimental facilities and ...
NASA Center: Glenn Research Center
Publication Year: 1991
Added to NTRS: 2008-05-31
Accession Number: 91N20093; Document ID: 19910010780
Experimental evaluation of corner turning vanes
Author(s): Moore, Royce D.; Boldman, Donald R.; Shyne, Rickey J.; Gelder, Thomas F.
Abstract: Two types of turning vane airfoils (a controlled-diffusion shape and a circular arc shape) have been evaluated in the high-speed and fan-drive corners of a 0.1-scale model of NASA Lewis Research Center's proposed Altitude ...
NASA Center: Glenn Research Center
Publication Year: 1987
Added to NTRS: 2005-10-13
Accession Number: 87N28571; Document ID: 19870019138; Report Number: E-3695, NAS 1.15:100143, NASA-TM-100143
Analysis and optimization of truncated scarf nozzles subject to external flow conditions
Author(s): Shyne, Rickey J.
Abstract: Results of a calculation of an optimized truncated scarfed nozzle were compared. The truncated scarfed nozzle was designed for an exit Mach number of 6.0, i.e., the Mach number at the last nozzle characteristic is 6.0, with ...
NASA Center: Glenn Research Center
Publication Year: 1988
Added to NTRS: 2005-10-13
Accession Number: 88N29746; Document ID: 19880020362; Report Number: E-4146, NAS 1.15:100955, NASA-TM-100955
Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
Author(s): Boldman, Donald R.; Moore, Royce D.; Shyne, Rickey J.
Abstract: Two turning vane designs were experimentally evaluated for corner 2 of a 0.1 scale model of the NASA Lewis Research Center's proposed Altitude Wind Tunnel (AWT). Corner 2 contained a simulated shaft fairing for a fan drive ...
NASA Center: Glenn Research Center
Publication Year: 1987
Added to NTRS: 2005-10-13
Accession Number: 87N18576; Document ID: 19870009143; Report Number: E-3175, NAS 1.60:2646, NASA-TP-2646
Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
Author(s): Moore, Royce D.; Shyne, Rickey J.; Boldman, Donald R.; Gelder, Thomas F.
Abstract: Detailed flow surveys downstream of the corner turning vanes and downstream of the fan inlet guide vanes have been obtained in a 0.1-scale model of the NASA Lewis Research Center's proposed Altitude Wind Tunnel. Two turning ...
NASA Center: Glenn Research Center
Publication Year: 1987
Added to NTRS: 2005-10-13
Accession Number: 87N20295; Document ID: 19870010862; Report Number: E-3294, NAS 1.60:2680, NASA-TP-2680
Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
Author(s): Shyne, Rickey J.; Keith, Theo G., Jr.
Abstract: Rao's method for computing optimum thrust nozzles is modified to study the effects of external flow on the performance of a class of exhaust nozzles. Members of this class are termed scarfed nozzles. These are ...
NASA Center: Glenn Research Center
Publication Year: 1990
Added to NTRS: 2005-08-25
Accession Number: 90N25106; Document ID: 19900015790; Report Number: AIAA PAPER 90-2222, E-5553, NAS 1.15:103175, NASA-TM-103175
Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
Author(s): Gelder, Thomas F.; Moore, Royce D.; Shyne, Rickey J.; Boldman, Donald R.
Abstract: Two turning vane designs were experimentally evaluated for the fan-drive corner (corner 2) coupled to an upstream diffuser and the high-speed corner (corner 1) of the 0.1 scale model of NASA Lewis Research Center's proposed ...
NASA Center: Glenn Research Center
Publication Year: 1987
Added to NTRS: 2005-08-25
Accession Number: 88N17686; Document ID: 19880008302; Report Number: E-3218, NAS 1.60:2681, NASA-TP-2681
Supersonic investigation of two dimensional hypersonic exhaust nozzles
Author(s): Carboni, Jeanne D.; Shyne, Rickey J.; Leavitt, Laurence D.; Taylor, John G.; Lamb, Milton
Abstract: An experimental investigation was conducted in the NASA Lewis 10 x 10 ft supersonic Wind Tunnel to determine the performance characteristics of 2D hypersonic exhaust nozzles/afterbodies at low supersonic conditions. ...
NASA Center: Glenn Research Center, Langley Research Center
Publication Year: 1992
Added to NTRS: 2005-08-25
Accession Number: 93N15342; Document ID: 19930006153; Report Number: E-7067, NAS 1.15:105687, NASA-TM-105687
Low Pressure Turbine Flow Physics Program
Author(s): Shyne, Rickey J.; Sohn, Ki-Hyeon
Abstract: As part of the collaborative NASA/industry/academia Low Pressure Turbine (LPT) Flow Physics program, smoke flow was visualized from a simulated low-pressure turbine experiment in NASA Lewis Research Center's CW-7 test ...
NASA Center: Glenn Research Center
Publication Year: 1997
Added to NTRS: 2005-08-25
Document ID: 20050177151
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