검색어 : 통합검색[Slater Glenn]
총 84건 중 84건 출력
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51
- Withdrawal: Refinement of Vortex Generators in a Streamline-Traced, External-Compression Supersonic Inlet
- Slater, John W.; NASA Glenn Research Center; (AIAA Scitech 2019 Forum, v.2019, 2019, )
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52
- Validation of WIND for a series of inlet flows
- Slater, J.; Abbott, J.; Cavicchi, R.; NASA, Glenn Research Center, Cleveland, OH; (40th AIAA Aerospace Sciences Meeting & Exhibit, v.2002, 2002, )
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53
- An Overview of Ensembl
- Birney, Ewan; Andrews, T. Daniel; Bevan, Paul; Caccamo, Mario; Chen, Yuan; Clarke, Laura; Coates, Guy; Cuff, James; Curwen, Val; Cutts, Tim; Down, Thomas; Eyras, Eduardo; Fernandez-Suarez, Xose M.; Gane, Paul; Gibbins, Brian; Gilbert, James; Hammond, Martin; Hotz, Hans-Rudolf; Iyer, Vivek; Jekosch, Kerstin; Kahari, Andreas; Kasprzyk, Arek; Keefe, Damian; Keenan, Stephen; Lehvaslaiho, Heikki; McVicker, Graham; Melsopp, Craig; Meidl, Patrick; Mongin, Emmanuel; Pettett, Roger; Potter, Simon; Proctor, Glenn; Rae, Mark; Searle, Steve; Slater, Guy; Smedley, Damian; Smith, James; Spooner, Will; Stabenau, Arne; Stalker, James; Storey, Roy; Ureta-Vidal, Abel; Woodwark, K. Cara; Cameron, Graham; Durbin, Richard; Cox, Anthony; Hubbard, Tim; Clamp, Michele; ; (Genome research, v.14, 2004, pp.925-928)
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54
- Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows
- Slater, John; NASA, Glenn Research Center, Cleveland, OH; (37th Joint Propulsion Conference and Exhibit, v.2001, 2001, )
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55
- Wave-Rotor Transition Duct Experiment
- Welch, Gerard; Slater, John; Wilson, Jack; U.S. Army Research Laboratory; NASA Glenn Research Center; QSS Group, Inc; (45th AIAA Aerospace Sciences Meeting and Exhibit, v.2007, 2007, )
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56
- Computing Aerodynamic Performance of 2-D Iced Airfoils with Structured Grids
- Zhu, Bin; Chi, Xingkai; Shih, Tom; Slater, John; Addy, H.; Choo, Yung; Michigan State University; Michigan State University; Michigan State University; NASA Glenn Research Center; NASA Glenn Research Center; NASA Glenn Research Center; (41st Aerospace Sciences Meeting and Exhibit, v.2003, 2003, )
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57
- Effect of Boundary-Layer Bleed Hole Inclination Angle and Scaling on Flow Coefficient Behavior
- Eichorn, Michael; Barnhart, Paul; Davis, David; Vyas, Manan; Slater, John; Case Western Reserve University; Case Western Reserve University; NASA Glenn Research Center; NASA Glenn Research Center; NASA Glenn Research Center; (51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, v.2013, 2013, )
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58
- Victoria's perioperative response to the COVID‐19 pandemic
- Watters, David A.; Brown, Wendy; Hardidge, Andrew; Foran, Paula; Holian, Annette; Jones, Michael; Kattula, Andrea; Radia‐ George, Camilla; Sawyer, Eleanor; Shedda, Susan; Slater, Ben; Wilson, Andew; Bourke, Joanne; Bouwer, Heinrich; Campbell, Graeme; Donald, Rebecca; Evans, Allison; Hore, Phillipa; Jeffreys, Andrew; McCahy, Philip; Pirpiris, Marinis; Spence, Denice; Story, David; Watson, Liat; Kenny, Sarah; Ryan‐ Atwood, Taliesin; Banting, Simon; Cashin, Paul; Chan, David; Crosthwaite, Gary; Dalton, David; Evans, Peter; Guest, Glenn D.; Sayed Hassen, A. H.; Hadfield, Matthew; McMurrick, Paul; O'Brien, Mike; O'Connell, Helen; Pitcher, Meron; Saunder, Alan; Sutherland, Alasdair; Thomas, Peter; Thomson, Benjamin N. J.; Williams, Simon; School of Medicine, Deakin University, Geelong, Victoria, Australia; Victorian Perioperative Consultative Council, Safer Care Victoria, Melbourne, Victoria, Australia; Department of Orthopaedic Surgery, Austin Health, Melbourne, Victoria, Australia; (ANZ journal of surgery, v.90, 2020, pp.1238-1241)
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59
- Improvements in Modeling 90-degree Bleed Holes for Supersonic Inlets
- Slater, John W.; NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44145; (Journal of propulsion and power, v.28, 2012, pp.773-781)
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60
- Modeling of Fixed-Exit Porous Bleed Systems for Supersonic Inlets
- Slater, John W.; Saunders, John D.; NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135; NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135; (Journal of propulsion and power, v.26, 2010, pp.193-202)
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