Flow Control on Bowed Compressor Cascades Using Vortex Generator Jet at Different Incidences-Reference-Cited by-同舟云学术

Flow Control on Bowed Compressor Cascades Using Vortex Generator Jet at Different Incidences

Published:2017-09 Issue:5 Volume:30 Page:04017028
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Li Longting¹,Song Yanping²,Chen Fu²,Meng Rui³

Affiliation:

1. Ph.D. Student, School of Energy Science and Engineering, Harbin Institute of Technology, Mailbox 458, No. 92, Xidazhi St., Nangang District, Harbin, Heilongjiang 150001, China (corresponding author).

2. Professor, School of Energy Science and Engineering, Harbin Institute of Technology, Mailbox 458, No. 92, Xidazhi St., Nangang District, Harbin, Heilongjiang 150001, China.

3. Master Student, School of Energy Science and Engineering, Harbin Institute of Technology, Mailbox 458, No. 92, Xidazhi St., Nangang District, Harbin, Heilongjiang 150001, 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.1943-5525.0000738

Reference37 articles.

1. Ball W. H. (1984). “Tests of wall blowing concepts for diffuser boundary layer control.” Proc. 20th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit American Institute of Aeronautics and Astronautics New York.

2. Parametric Optimization of Unsteady End Wall Blowing on a Highly Loaded Low-Pressure Turbine

3. Secondary Flow Loss Reduction Through Blowing for a High-Lift Front-Loaded Low Pressure Turbine Cascade

4. CFX [Computer software]. ANSYS Pittsburgh.

5. Chen S. W. (2007). “Experimental and numerical investigation of using bowed blade in compressor cascade with different turbine angles.” Ph.D. thesis Harbin Institute of Technology Harbin China (in Chinese).

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