검색어 : 통합검색[Slater Glenn]
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71
- Axisymmetric Turbulent Shockwave Boundary Layer Interaction at Mach 2.5
- Mosele, John-Paul G.; Gross, Andreas; Slater, John W.; New Mexico State University; New Mexico State University; NASA Glenn Research Center; (AIAA AVIATION 2020 FORUM, v.2020, 2020, )
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72
- Panel Flutter Model Identification Using the Minimum Model Error Method on the Forced Response Measurements
- Shiryayev, Oleg V.; Slater, Joseph C.; Department of Mechanical and Materials Engineering, Wright State University, 3640 Colonel Glenn Hwy., Dayton, OH 45435; Department of Mechanical and Materials Engineering, Wright State University, 3640 Colonel Glenn Hwy., Dayton, OH 45435; (Journal of vibration and acoustics, v.128, 2006, pp.635-645)
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73
- Computing Aerodynamic Performance of 2D Iced Airfoils: Blocking Strategy and Convergence Rate
- Zhu, Bin; Chi, Kyle; Shih, Tom; Slater, John; Michigan State University; Michigan State University; Michigan State University; NASA Glenn Research Center; (20th AIAA Applied Aerodynamics Conference, v.2002, 2002, )
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74
- Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions
- Schwartz, Matthew J.; Gaitonde, Datta V.; Slater, John W.; The Ohio State University, Columbus, Ohio 43210; The Ohio State University, Columbus, Ohio 43210; NASA Glenn Research Center, Cleveland, Ohio 44145; (Journal of propulsion and power, v.39, 2023, pp.106-120)
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75
- Improved structural damage identification using random decrement signatures: Application to FEM data
- Shiryayev, Oleg V.; Slater, Joseph C.; Department of Mechanical and Materials Engineering, 209 Russ Engineering Center, Wright State University, 3640 Colonel Glenn Hwy., Dayton, OH 45435, U.S.A.; Department of Mechanical and Materials Engineering, 209 Russ Engineering Center, Wright State University, 3640 Colonel Glenn Hwy., Dayton, OH 45435, U.S.A.; (Structural control and health monitoring, v.15, 2008, pp.1006-1020)
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76
- Computing aerodynamic performance of a 2D iced airfoil - Blocking topology and grid generation
- Chi, X.; Slater, J.; Shih, T.; Zhu, B.; Addy, H.; Choo, Y.; Michigan State Univ., East Lansing; NASA, Glenn Research Center, Cleveland, OH; (40th AIAA Aerospace Sciences Meeting & Exhibit, v.2002, 2002, )
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77
- Implementation of a Compressor Face Boundary Condition Based on Small Disturbances
- Slater, John W.; Paynter, Gerald C.; John H. Glenn Research Center at Lewis Field, MS 86-7, 21000 Brookpark Road, Cleveland, OH 44135; The Boeing Company, MS 67-LF P.O. Box 3707, Seattle, WA 98124; (Journal of turbomachinery, v.123, 2001, pp.386-391)
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78
- Vortex Generators in a Two-Dimensional External-Compression Supersonic Inlet
- Baydar, Ezgihan; Lu, Frank K.; Slater, John W.; University of Texas at Arlington, Arlington, Texas 76019; University of Texas at Arlington, Arlington, Texas 76019; NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135; (Journal of propulsion and power, v.34, 2018, pp.521-538)
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79
- Ensembl’s 10th year
- Flicek, Paul; Aken, Bronwen L.; Ballester, Benoit; Beal, Kathryn; Bragin, Eugene; Brent, Simon; Chen, Yuan; Clapham, Peter; Coates, Guy; Fairley, Susan; Fitzgerald, Stephen; Fernandez-Banet, Julio; Gordon, Leo; Grä f, Stefan; Haider, Syed; Hammond, Martin; Howe, Kerstin; Jenkinson, Andrew; Johnson, Nathan; Kä hä ri, Andreas; Keefe, Damian; Keenan, Stephen; Kinsella, Rhoda; Kokocinski, Felix; Koscielny, Gautier; Kulesha, Eugene; Lawson, Daniel; Longden, Ian; Massingham, Tim; McLaren, William; Megy, Karine; Overduin, Bert; Pritchard, Bethan; Rios, Daniel; Ruffier, Magali; Schuster, Michael; Slater, Guy; Smedley, Damian; Spudich, Giulietta; Tang, Y. Amy; Trevanion, Stephen; Vilella, Albert; Vogel, Jan; White, Simon; Wilder, Steven P.; Zadissa, Amonida; Birney, Ewan; Cunningham, Fiona; Dunham, Ian; Durbin, Richard; Ferná ndez-Suarez, Xosé M.; Herrero, Javier; Hubbard, Tim J. P.; Parker, Anne; Proctor, Glenn; Sm; European Bioinformatics Institute, Wellcome Trust Genome Campus, Hinxton Cambridge CB10 1SD and Wellcome Trust Sanger Institute, Wellcome Trust Genome Campus, Hinxton, Cambridge, CB10 1SA, UK; European Bioinformatics Institute, Wellcome Trust Genome Campus, Hinxton Cambridge CB10 1SD and Wellcome Trust Sanger Institute, Wellcome Trust Genome Campus, Hinxton, Cambridge, CB10 1SA, UK; European Bioinformatics Institute, Wellcome Trust Genome Campus, Hinxton Cambridge CB10 1SD and Wellcome Trust Sanger Institute, Wellcome Trust Genome Campus, Hinxton, Cambridge, CB10 1SA, UK; European Bioinformatics Institute, Wellcome Trust Genome Campus, Hinxton Cambridge CB10 1SD and Wellcome Trust Sanger Institute, Wellcome Trust Genome Campus, Hinxton, Cambridge, CB10 1SA, UK; European Bioinformatics Institute, Wellcome Trust Genome Campus, Hinxton Cambridge CB10 1SD and Wellcome Trust Sanger Institute, Wellcome Trust Genome Campus, Hinxton, Cambridge, CB10 1SA, UK; European Bioinformatics Instit; (Nucleic acids research, v.38, 2010, pp.D557-D562)
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80
- Redesign of the B-1B Bomber Inlets for Improved Supersonic Performance
- Berra, Lee M.; Olcmen, Semih; Slater, John W.; United States Air Force and the University of Alabama, Tuscaloosa, AL; The University of Alabama, Tuscaloosa, AL; NASA John H. Glenn Research Center, Cleveland, OH; (Volume 1: Advances in Aerospace Technology, v.2014, 2014, pp.V001T01A062)
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