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Published/Copyright: December 13, 2012

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"Masthead" Int. J. Turbo Jet-Engines, vol. 29, no. 4, 2012, pp. iii-iii. https://doi.org/10.1515/tjj-2012-masthead4

(2012). Masthead. Int. J. Turbo Jet-Engines, 29(4), iii-iii. https://doi.org/10.1515/tjj-2012-masthead4

(2012) Masthead. Int. J. Turbo Jet-Engines, Vol. 29 (Issue 4), pp. iii-iii. https://doi.org/10.1515/tjj-2012-masthead4

"Masthead" Int. J. Turbo Jet-Engines 29, no. 4 (2012): iii-iii. https://doi.org/10.1515/tjj-2012-masthead4

Masthead. Int. J. Turbo Jet-Engines. 2012;29(4): iii-iii. https://doi.org/10.1515/tjj-2012-masthead4

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Published Online: 2012-12-13

Published in Print: 2012-12-18

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Masthead
Flow Field around a Blunt-nosed Body with Spike
The Flow Analysis and Performance Improvement of the Flow Return System in High Pressure Fans
Numerical Investigation of Heat Transfer Characteristic on Scalelike Platelet Inner Duct
Analytical Calculation of Stall-inception and Surge Points for an Axial-flow Compressor Rotor
Fatigue Life Estimation of an Aircaft Engine Under Different Load Spectrums
Numerical Simulation of Tangling in Jet Engine Turbines
Statistical Turbofan Architecture Management for Use in a Supercirculation Wing Aircraft
Calculating High Speed Centrifugal Compressor Performance from Averaged Measurements
Preliminary Experimental Investigation on Detonation Initiation in the Ejector of a Pulse Detonation Rocket Engine
An Application of Fuzzy Fault Tree Analysis to Uncontained Events of an Areo-Engine Rotor

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Masthead
Flow Field around a Blunt-nosed Body with Spike
The Flow Analysis and Performance Improvement of the Flow Return System in High Pressure Fans
Numerical Investigation of Heat Transfer Characteristic on Scalelike Platelet Inner Duct
Analytical Calculation of Stall-inception and Surge Points for an Axial-flow Compressor Rotor
Fatigue Life Estimation of an Aircaft Engine Under Different Load Spectrums
Numerical Simulation of Tangling in Jet Engine Turbines
Statistical Turbofan Architecture Management for Use in a Supercirculation Wing Aircraft
Calculating High Speed Centrifugal Compressor Performance from Averaged Measurements
Preliminary Experimental Investigation on Detonation Initiation in the Ejector of a Pulse Detonation Rocket Engine
An Application of Fuzzy Fault Tree Analysis to Uncontained Events of an Areo-Engine Rotor