Numerical and Experimental Investigations on Windage Heating Effect of Labyrinth Seals-Reference-Cited by-同舟云学术

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Numerical and Experimental Investigations on Windage Heating Effect of Labyrinth Seals

Published:2020-09 Issue:5 Volume:33 Page:04020057
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sun Dan¹,Zhou Min²,Zhao Huan¹,Lu Jiang²,Fei Cheng-Wei³^ORCID,Li Huan⁴

Affiliation:

1. Professor, Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System, Shenyang Aerospace Univ., Shenyang 110136, PR China.

2. Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System, Shenyang Aerospace Univ., Shenyang 110136, PR China.

3. Professor, Dept. of Aeronautics and Astronautics, Fudan Univ., Shanghai 200433, PR China (corresponding author). ORCID: .

4. M.Sc. Student, Dept. of Aeronautics and Astronautics, Fudan Univ., Shanghai 200433, PR 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.1943-5525.0001175

Reference23 articles.

1. Sealing in Turbomachinery

2. Evaluation of the Turbulence Model Influence on the Numerical Simulations of Unsteady Cavitation

3. Delgado I. R. and M. P. Proctor. 2006. “Continue investigation of leakage and power loss test results for competing turbine engine seals.” In Proc. 42nd Joint Propulsion Conf. and Exhibit. Sacramento CA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4754.

4. Denecke J. K. Dullenkopf S. Wittig and H. J. Bauer. 2005a. “Experimental investigation of the total temperature increase and swirl development in rotating labyrinth seals.” In Vol. 3 of Proc. ASME Turbo Expo 2005: Power for Land Sea and Air 1161–1171. Reno NV: International Gas Turbine Institute. https://asmedigitalcollection.asme.org/GT/proceedings-abstract/GT2005/47268/1161/312940.

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