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Results 1 to 25 of 202268

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POWERING aheadLANGSTON, ByleeS.Mechanical engineering (New York, N.Y. 1919). 2011, Vol 133, Num 5, pp 30-33, issn 0025-6501, 4 p.Article

Simulation des performances d'une turbine helicoradiale de suralimentation = Simulation on the performance of a small supercharging turbineDESCOMBES, G; DUAN, Q; JULLIEN, J et al.R.F.M. Revue française de mécanique. 1998, Num 2, pp 99-106, issn 0373-6601Conference Paper

Grossmotorenforschung an der Technischen Universität Graz = Research on large motors at the Technical University in GrazWIMMER, Andreas.ÖIAZ. 2003, Vol 148, Num 4, pp 133-136, issn 0721-9415, 4 p.Article

Architecture of functionally graded ceramic coatings against surface thermal fractureCHOULES, B. D; KOKINI, K.Journal of engineering materials and technology. 1996, Vol 118, Num 4, pp 522-528, issn 0094-4289Article

Effect of Fatigue on Proof Strength of Gas Turbine Combustor CasingSARANGI, Niranjan; PANIGRAHI, S. K; PATEL, S. K et al.Journal of failure analysis and prevention. 2013, Vol 13, Num 1, pp 102-111, issn 1547-7029, 10 p.Article

Experimental investigation of droplet size influence on low pressure steam turbine blade erosionAHMAD, M; SCHATZ, M; CASEY, M. V et al.Wear. 2013, Vol 303, Num 1-2, pp 83-86, issn 0043-1648, 4 p.Article

Effect of Pulsed Film Cooling on Leading Edge Film EffectivenessEI-GABRY, Lamyaa A; RIVIR, Richard B.Journal of turbomachinery. 2012, Vol 134, Num 4, issn 0889-504X, 041005.1-041005.6Article

A multi-regulator sliding mode control strategy for output-constrained systemsRICHTER, Hanz.Automatica (Oxford). 2011, Vol 47, Num 10, pp 2251-2259, issn 0005-1098, 9 p.Article

A free-jet experimental study on the performance of a cavity-type ramjetJIANGUO TAN; YU PAN; JIANHAN LIANG et al.Journal of mechanical science and technology. 2011, Vol 25, Num 11, pp 2951-2957, issn 1738-494X, 7 p.Article

Study on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft EnginesFUJIMOTO, Shu; OKITA, Yoji; FUKUYAMA, Yoshitaka et al.Journal of turbomachinery. 2010, Vol 132, Num 3, issn 0889-504X, 031019.1-031019.10Article

Suction-Side Gill Region Film Cooling: Effects of Hole Shape and Orientation on Adiabatic Effectiveness and Heat Transfer CoefficientCHAPPELL, Justin; LIGRANI, Phil; SREEKANTH, Sri et al.Journal of turbomachinery. 2010, Vol 132, Num 3, issn 0889-504X, 031022.1-031022.11Article

Defect diagnostics of gas turbine engine using hybrid SVM-ANN with module system in off-design conditionSEO, Dong-Hyuck; ROH, Tae-Seong; CHOI, Dong-Whan et al.Journal of mechanical science and technology. 2009, Vol 23, Num 3, pp 677-685, issn 1738-494X, 9 p.Article

Effect of End Wall Contouring on Performance of Ultra-Low Aspect Ratio Transonic Turbine Inlet Guide VanesSONODA, Toyotaka; HASENJÄGER, Martina; ARIMA, Toshiyuki et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 011020.1-011020.11Article

Endwall Boundary Layer Development in an Engine Representative Four-Stage Low Pressure Turbine RigVERA, Maria; DE LA ROSA BLANCO, Elena; HODSON, Howard et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 011017.1-011017.9Article

Experimental Investigation of the Clocking Effect in a 1.5-Stage Axial Turbine-Part II: Unsteady Results and Boundary Layer BehaviorKÖNIG, Sven; STOFFEL, Bernd; TAHER SCHOBEIRI, M et al.Journal of turbomachinery. 2009, Vol 131, Num 2, issn 0889-504X, 021004.1-021004.8Article

Interstage Flow Interactions and Loss Generation in a Two-Stage Shrouded Axial TurbinePORRECA, L; KALFAS, A. I; ABHARI, R. S et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 11002.1-011002.12Article

Heat Transfer Coefficients of Film Cooling on a Rotating Turbine Blade Model-Part I: Effect of Blowing RatioZHI TAO; ZHENMING ZHAO; SHUITING DING et al.Journal of turbomachinery. 2009, Vol 131, Num 4, issn 0889-504X, 041005.1-041005.12Article

Integration of thermomechanical strains into tolerancing analysisPIERRE, Laurent; TEISSANDIER, Denis; NADEAU, Jean Pierre et al.IJIDEM. 2009, Vol 3, Num 4, pp 247-263, issn 1955-2513, 17 p.Article

Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness on a Gas Turbine Blade TipMHETRAS, Shantanu; NARZARY, Diganta; ZHIHONG GAO et al.Journal of turbomachinery. 2008, Vol 130, Num 2, issn 0889-504X, 021002.1-021002.13Article

Internal Cooling Near Trailing Edge of a Gas Turbine Airfoil With Cooling Airflow Through Blockages With HolesLAU, S. C; CERVANTES, J; HAN, J. C et al.Journal of turbomachinery. 2008, Vol 130, Num 3, issn 0889-504X, 031004.1-031004.9Article

Optimized Shroud Design for Axial Turbine Aerodynamic PerformancePORRECA, L; KALFAS, A. I; ABHARI, R. S et al.Journal of turbomachinery. 2008, Vol 130, Num 3, issn 0889-504X, 031016.1-031016.12Article

The Influence of Shroud and Cavity Geometry on Turbine Performance: An Experimental and Computational Study-Part I: Shroud GeometryROSIC, Budimir; DENTON, John D; CURTIS, Eric M et al.Journal of turbomachinery. 2008, Vol 130, Num 4, issn 0889-504X, 041001.1-041001.10Article

Propulsion à plasma : vers de nouveaux concepts pour les missions du futur : Electrotechnique du futur = Plasma Propulsion : Towards New Concepts for Future MissionsGARRIGUES, Laurent; PEREZ-LUNA, Jaime; HAGELAAR, Gerjan J. M et al.REE. Revue de l'électricité et de l'électronique. 2008, Num 4, issn 1265-6534, 53-59, 68 [8 p.]Article

Advanced modeling of underplatform friction dampers for analysis of bladed disk vibrationPETROV, E. P; EWINS, D. J.Journal of turbomachinery. 2007, Vol 129, Num 1, pp 143-150, issn 0889-504X, 8 p.Article

Aeroelastic stability of welded-in-pair low pressure turbine rotor blades : A comparative study using linear methodsCORRAL, Roque; GALLARDO, Juan Manuel; VASCO, Carlos et al.Journal of turbomachinery. 2007, Vol 129, Num 1, pp 72-83, issn 0889-504X, 12 p.Article

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