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Published/Copyright: August 4, 2017

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"Frontmatter" International Journal of Turbo & Jet-Engines, vol. 34, no. 3, 2017, pp. i-iii. https://doi.org/10.1515/tjj-2017-frontmatter3

(2017). Frontmatter. International Journal of Turbo & Jet-Engines, 34(3), i-iii. https://doi.org/10.1515/tjj-2017-frontmatter3

(2017) Frontmatter. International Journal of Turbo & Jet-Engines, Vol. 34 (Issue 3), pp. i-iii. https://doi.org/10.1515/tjj-2017-frontmatter3

"Frontmatter" International Journal of Turbo & Jet-Engines 34, no. 3 (2017): i-iii. https://doi.org/10.1515/tjj-2017-frontmatter3

Frontmatter. International Journal of Turbo & Jet-Engines. 2017;34(3): i-iii. https://doi.org/10.1515/tjj-2017-frontmatter3

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Published Online: 2017-8-4

Published in Print: 2017-8-3

Articles in the same Issue

Frontmatter
Effects of Cavity Configurations on Flameholding and Performances of Kerosene Fueled Scramjet Combustor
Metaheuristic and Machine Learning Models for TFE-731-2, PW4056, and JT8D-9 Cruise Thrust
Design Optimization Method for Composite Components Based on Moment Reliability-Sensitivity Criteria
Use Deflected Trailing Edge to Improve the Aerodynamic Performance and Develop Low Solidity LPT Cascade
A Co-modeling Method Based on Component Features for Mechatronic Devices in Aero-engines
Evaluation and Analysis of Curvature-Corrected Filter-based Turbulent Model
Aircraft Engine Thrust Estimator Design Based on GSA-LSSVM
Effect of Inner Nozzle Lip Thickness on Co-flow Jet Characteristics
Comparisons of Two Non-probabilistic Structural Reliability Analysis Methods for Aero-engine Turbine Disk

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Frontmatter
Effects of Cavity Configurations on Flameholding and Performances of Kerosene Fueled Scramjet Combustor
Metaheuristic and Machine Learning Models for TFE-731-2, PW4056, and JT8D-9 Cruise Thrust
Design Optimization Method for Composite Components Based on Moment Reliability-Sensitivity Criteria
Use Deflected Trailing Edge to Improve the Aerodynamic Performance and Develop Low Solidity LPT Cascade
A Co-modeling Method Based on Component Features for Mechatronic Devices in Aero-engines
Evaluation and Analysis of Curvature-Corrected Filter-based Turbulent Model
Aircraft Engine Thrust Estimator Design Based on GSA-LSSVM
Effect of Inner Nozzle Lip Thickness on Co-flow Jet Characteristics
Comparisons of Two Non-probabilistic Structural Reliability Analysis Methods for Aero-engine Turbine Disk