Blade Design and Thrust Performance for a Miniature Turbojet Engine

Bor-Jang Tsai,; Hsiao-Wei Chiang,; Yu-Shan Luo,

doi:10.1515/TJJ.2006.23.3.137

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Blade Design and Thrust Performance for a Miniature Turbojet Engine

Bor-Jang Tsai, , Hsiao-Wei Chiang, and Yu-Shan Luo,

Published/Copyright: September 1, 2006

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From the journal International Journal of Turbo and Jet Engines Volume 23 Issue 3

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Harvard
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Vancouver

Tsai,, Bor-Jang, Chiang,, Hsiao-Wei and Luo,, Yu-Shan. "Blade Design and Thrust Performance for a Miniature Turbojet Engine" International Journal of Turbo and Jet Engines, vol. 23, no. 3, pp. 137-154. https://doi.org/10.1515/TJJ.2006.23.3.137

Tsai,, B., Chiang,, H. & Luo,, Y. (). Blade Design and Thrust Performance for a Miniature Turbojet Engine. International Journal of Turbo and Jet Engines, 23(3), 137-154. https://doi.org/10.1515/TJJ.2006.23.3.137

Tsai,, B., Chiang,, H. and Luo,, Y. () Blade Design and Thrust Performance for a Miniature Turbojet Engine. International Journal of Turbo and Jet Engines, Vol. 23 (Issue 3), pp. 137-154. https://doi.org/10.1515/TJJ.2006.23.3.137

Tsai,, Bor-Jang, Chiang,, Hsiao-Wei and Luo,, Yu-Shan. "Blade Design and Thrust Performance for a Miniature Turbojet Engine" International Journal of Turbo and Jet Engines 23, no. 3 (): 137-154. https://doi.org/10.1515/TJJ.2006.23.3.137

Tsai, B, Chiang, H, Luo, Y. Blade Design and Thrust Performance for a Miniature Turbojet Engine. International Journal of Turbo and Jet Engines. ;23(3): 137-154. https://doi.org/10.1515/TJJ.2006.23.3.137

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Articles in the same Issue

CONTENTS
Blade Design and Thrust Performance for a Miniature Turbojet Engine
A Numerical Study on Passive Control of Cavity Induced Pressure Oscillations in Two-Dimensional Supersonic Flow
Nonlinear Oscillations in Compressor under Rotating Inlet Distortions
CFD Prediction of Supersonic Ejectors Performance
Probabilistic Analysis of Gas Turbine Field Performance
High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows

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https://doi.org/10.1515/TJJ.2006.23.3.137

Articles in the same Issue

CONTENTS
Blade Design and Thrust Performance for a Miniature Turbojet Engine
A Numerical Study on Passive Control of Cavity Induced Pressure Oscillations in Two-Dimensional Supersonic Flow
Nonlinear Oscillations in Compressor under Rotating Inlet Distortions
CFD Prediction of Supersonic Ejectors Performance
Probabilistic Analysis of Gas Turbine Field Performance
High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows