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Published/Copyright: November 27, 2014

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"Frontmatter" International Journal of Turbo & Jet-Engines, vol. 31, no. 4, 2014, pp. i-iii. https://doi.org/10.1515/tjj-2014-frontmatter4

(2014). Frontmatter. International Journal of Turbo & Jet-Engines, 31(4), i-iii. https://doi.org/10.1515/tjj-2014-frontmatter4

(2014) Frontmatter. International Journal of Turbo & Jet-Engines, Vol. 31 (Issue 4), pp. i-iii. https://doi.org/10.1515/tjj-2014-frontmatter4

"Frontmatter" International Journal of Turbo & Jet-Engines 31, no. 4 (2014): i-iii. https://doi.org/10.1515/tjj-2014-frontmatter4

Frontmatter. International Journal of Turbo & Jet-Engines. 2014;31(4): i-iii. https://doi.org/10.1515/tjj-2014-frontmatter4

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Published Online: 2014-11-27

Published in Print: 2014-12-1

Articles in the same Issue

Frontmatter
Editorial on Future Jet Technologies
Design and Numerical Simulation of Radial Inflow Turbine Volute
Investigation about Rotor-stator Interaction with an Adjustable Leaned Vane Blade
Burning Rate of Composite Propellants under the Conditions of Strain
The Effects of Blade 3D Designs in Different Orthogonal Coordinates on the Performance of Compressor Cascades
Numerical Study of a Boundary Layer Bleedfor a Rocket-Based Combined-Cycle Inlet in Ejector Mode
Effect of Rotation on Flow Field and Film Cooling Effectiveness in Film-Cooled Turbine Rotors
Frequency-domain Model Matching PID Controller Design for Aero-engine

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Frontmatter
Editorial on Future Jet Technologies
Design and Numerical Simulation of Radial Inflow Turbine Volute
Investigation about Rotor-stator Interaction with an Adjustable Leaned Vane Blade
Burning Rate of Composite Propellants under the Conditions of Strain
The Effects of Blade 3D Designs in Different Orthogonal Coordinates on the Performance of Compressor Cascades
Numerical Study of a Boundary Layer Bleedfor a Rocket-Based Combined-Cycle Inlet in Ejector Mode
Effect of Rotation on Flow Field and Film Cooling Effectiveness in Film-Cooled Turbine Rotors
Frequency-domain Model Matching PID Controller Design for Aero-engine