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Results 1 to 25 of 7075

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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

Environmental degradation of thermal-barrier coatings by molten deposits : Thermal-Barrier Coatings for More Efficient Gas-Turbine EnginesLEVI, Carlos G; HUTCHINSON, John W; VIDAL-SETIF, Marie-Hélène et al.MRS bulletin. 2012, Vol 37, Num 10, pp 932-941, issn 0883-7694, 10 p.Article

Processing science of advanced thermal-barrier systems : Thermal-Barrier Coatings for More Efficient Gas-Turbine EnginesSAMPATH, Sanjay; SCHULZ, Uwe; JARLIGO, Maria Ophelia et al.MRS bulletin. 2012, Vol 37, Num 10, pp 903-910, issn 0883-7694, 8 p.Article

Testing and evaluation of thermal-barrier coatings : Thermal-Barrier Coatings for More Efficient Gas-Turbine EnginesVASSEN, Robert; KAGAWA, Yutaka; SUBRAMANIAN, Ramesh et al.MRS bulletin. 2012, Vol 37, Num 10, pp 911-916, issn 0883-7694, 6 p.Article

Detection and numerical analysis of the most efforted places in turbine blades under real working conditionsSADOWSKI, Tomasz; GOLEWSKI, Przemystaw.Computational materials science. 2012, Vol 64, pp 285-288, issn 0927-0256, 4 p.Conference Paper

Vaneless Diffuser Advanced ModelDUBITSKY, Oleg; JAPIKSE, David.Journal of turbomachinery. 2008, Vol 130, Num 1, issn 0889-504X, 011020.1-011020.10Article

Coriolis forces in forced response analysis of mistuned bladed disksNIKOLIC, M; PETROV, E. P; EWINS, D. J et al.Journal of turbomachinery. 2007, Vol 129, Num 4, pp 730-739, issn 0889-504X, 10 p.Article

A diesel-electric submarine propulsion simulation. DiscussionBOWKER, M. A; HAINES, N. A; PENROSE, G. S et al.Transactions - Institute of Marine Engineers (1988). 1991, Vol 103, pp 255-267, issn 1358-3956, 5Article

Green light to plastic engine partsBAXTER, D. F.Advanced materials & processes. 1991, Vol 139, Num 5, pp 26-31, issn 0882-7958Article

The silence of the fansSTEVENS, T.Materials engineering. 1991, Vol 108, Num 8, pp 21-24, issn 0025-5319Article

A Passive Reaction Force Compensation (RFC) Mechanism for a Linear Motor Motion StageYOU, Yo-Han; AHN, Hyeong-Joon.International journal of precision engineering and manufacturing. 2014, Vol 15, Num 5, pp 797-801, 5 p.Article

Rotordynamic Modelling and Analysis of a Radial Inflow Turbine Rotor-Bearing SystemJUNG, Hyung-Chul; KRUMDIECK, Susan.International journal of precision engineering and manufacturing. 2014, Vol 15, Num 11, pp 2285-2290, 6 p.Article

Piston ring and cylinder liner wear aggravation caused by transition to greener ship transports-Comparison of samples from test rig and fieldOLANDER, P; HOLLMAN, P; JACOBSON, S et al.Wear. 2013, Vol 302, Num 1-2, pp 1345-1350, issn 0043-1648, 6 p.Conference Paper

Analysis of the Variable Geometry Effect in Radial TurbinesBINDER, Nicolas; LE GUYADER, Sebastien; CARBONNEAU, Xavier et al.Journal of turbomachinery. 2012, Vol 134, Num 4, issn 0889-504X, 041017.1-041017.9Article

A simplified method for predicting the stability of aerodynamically excited turbomachinerySTORACE, Albert F.Journal of turbomachinery. 2007, Vol 129, Num 4, pp 724-729, issn 0889-504X, 6 p.Article

Effects of bleed rate and endwall location on the aerodynamic behavior of a circular hole bleed off-takeLEISHMAN, B. A; CUMPSTY, N. A; DENTON, J. D et al.Journal of turbomachinery. 2007, Vol 129, Num 4, pp 645-658, issn 0889-504X, 14 p.Article

Stepping motor for use in uhvKUSUNOKI, I; SATOMI, H; KOBORI, M et al.Vacuum. 1990, Vol 41, Num 7-9, pp 1946-1947, issn 0042-207XConference Paper

Shape design sensitivity analysis of an axisymmetric turbine disk using the boundary element methodPARK, C. W; YOO, Y. M; KWON, K. H et al.Computers & structures. 1989, Vol 33, Num 1, pp 7-16, issn 0045-7949, 10 p.Article

Numerical investigation on laser stripping of thermal barrier coatingMARIMUTHU, S; KAMARA, A. M; SEZER, H. K et al.Computational materials science. 2014, Vol 88, pp 131-138, issn 0927-0256, 8 p.Article

Failure Analysis of HP Turbine Blades in a Low Bypass Turbofan EngineMISHRA, R. K; JOHNEY, Thomas; SRINIVASAN, K et al.Journal of failure analysis and prevention. 2013, Vol 13, Num 3, pp 274-281, issn 1547-7029, 8 p.Article

Momionctional coating interlayers for thermal-barrier systems : Thermal-Barrier Coatings for More Efficient Gas-Turbine EnginesPOLLOCK, T. M; LIPKIN, D. M; HEMKER, K. J et al.MRS bulletin. 2012, Vol 37, Num 10, pp 923-931, issn 0883-7694, 9 p.Article

Coupled Axisymmetric Finite Element Model of a Magneto-hydraulic Actuator for Active Engine MountsCHAKRABARTI, Suryarghya; DAPINO, Marcelo J.Proceedings of SPIE, the International Society for Optical Engineering. 2011, Vol 7979, issn 0277-786X, isbn 978-0-8194-8541-0, 79790C.1-79790C.13Conference Paper

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