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A Numerical Investigation on the Influence of Film-Cooling Hole Inclination Angle on the Stress Field of Surrounding Thermal Barrier Coating. [PDF]
Shi Z, Jia Y, He X, Tian Z, Liu Y.
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Techno-economic study of gas turbines with hydrogen, ammonia, and their mixture fuels. [PDF]
Yazdani AM, Salimi M, Amidpour M.
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Onboard power systems based on hot water energy storage for green vehicles as an alternative to battery electric vehicles. [PDF]
Cao Y.
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Digital Fuel Control for a Lean Premixed Hydrogen-Fueled Gas Turbine Engine
Daniel Christopher Villarreal
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Thermodynamic investigation of the efficiency of ammonia-powered marine solid oxide fuel cells with gas turbine. [PDF]
Serbin S +3 more
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Review of Non-Destructive Testing for Wind Turbine Bolts. [PDF]
Sun H +8 more
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Aircraft Engineering and Aerospace Technology, 1974
THE SCOPE of Rolls‐Royce (1971) Limited's operation and its international and North American activities can be best understood by a look at some vital statistics.
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THE SCOPE of Rolls‐Royce (1971) Limited's operation and its international and North American activities can be best understood by a look at some vital statistics.
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1981
In order to minimise fuel consumption and increase thrust, the operating temperatures of aero engine gas turbines have increased significantly over the last 30 years.
D. Driver, D. W. Hall, G. W. Meetham
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In order to minimise fuel consumption and increase thrust, the operating temperatures of aero engine gas turbines have increased significantly over the last 30 years.
D. Driver, D. W. Hall, G. W. Meetham
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A Computational Method For Gas Turbine Engines
43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005Designing and developing new aerospace propulsion systems is time-consuming and expensive. Computational simulation is a promising means for alleviating this, due to the flexibility it provides for rapid and relatively inexpensive evaluation of alternative designs, and because it can be used to integrate multidisciplinary analysis earlier in the design
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