Investigation of the Stability Criterion for Axial Compressor under Circumferential Total Pressure Distortion-Reference-Cited by-同舟云学术

Investigation of the Stability Criterion for Axial Compressor under Circumferential Total Pressure Distortion

Published:2023-09 Issue:5 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Xu Haoyang¹^ORCID,Hu Jun²,Guo Jin³

Affiliation:

1. Ph.D. Student, Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Yudao St., Qinhuai District, Nanjing 210016, China (corresponding author). ORCID: .

2. Professor, Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Yudao St., Qinhuai District, Nanjing 210016, China.

3. Ph.D. Student, Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Yudao St., Qinhuai District, Nanjing 210016, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4419

Reference18 articles.

1. Daniele C. J. and F. Teren. 1975. “Prediction of compressor stall for distorted and undistorted flow by use of a multistage compressor simulation on the digital computer.” In Proc. AIAA 13th Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics.

2. Stall, Surge, and 75 Years of Research

3. Dunham, J. 1965. “Non-axisymmetric flows in axial compressors.” In Institution of mechanical engineers, mechanical engineering science monograph No. 3. New York: ASME.

4. Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System Model

5. Surge and Rotating Stall in Axial Flow Compressors—Part II: Experimental Results and Comparison With Theory