Shock System Model of Highly Loaded Turbine Cascade-Reference-Cited by-同舟云学术

Shock System Model of Highly Loaded Turbine Cascade

Published:2020-01 Issue:1 Volume:33 Page:04019107
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhou ZhiHong¹^ORCID,Liu HuoXing²,Zhou Kun³,Li Chao⁴

Affiliation:

1. Ph.D. Candidate, School of Energy and Power Engineering, Beihang Univ., Beijing 100083, China. ORCID: .

2. Professor, School of Energy and Power Engineering, Beihang Univ., Beijing 100083, China (corresponding author).

3. Aero Engine Academy of China, No. 21, Shunxing Rd., Shunyi, Beijing 101300, China.

4. Master of Engineering, School of Energy and Power Engineering, Beihang Univ., Beijing 100083, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001095

Reference20 articles.

1. The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines

2. The Trailing Edge Loss of Transonic Turbine Blades

3. A Study of the Effects of Tip Clearance in a Supersonic Turbine

4. Giel P. W. 2008. “NASA/GE highly-loaded turbine research program.” In Proc. NASA Fundamental Aeronautics 2007 Annual Meeting. Washington DC: National Aeronautics and Space Administration.

5. Profile losses prediction of transonic turbine cascades;Gong J. B.;Turbine Technol.,2009

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