Unstructured Grid Technology Applied to Axial-flow Compressors-Reference-Cited by-同舟云学术

Unstructured Grid Technology Applied to Axial-flow Compressors

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Webster Robert¹,Hyams D¹,Sreenivas K¹

Affiliation:

1. University of Tennessee, Chattanooga

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1605

Reference29 articles.

1. 1Janus, J.M. "Advanced 3-D CFD Algorithm for Turbomachinery," Ph.D Dissertation,Mississippi State University, MS, 1989.

2. 2Chen, J-P, "Unsteady Three-Dimensional Thin-Layer Navier-Stokes Solutions for Turbomachinery in Transonic Flow," Ph.D. Dissertation,MississippiState University,MS,1991.

3. Comparison of computations using Navier-Stokes equations in rotating and fixed coordinates for flow through turbomachinery

4. A New Procedure for Simulating Unsteady Flows Through Turbomachinery Blade Passages

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Influence of External Factors on Airborne Missile’s Horizontal Backward Launching;International Journal of Aerospace Engineering;2021-08-22

2. Study on Initial Disturbance of Airborne Missile’s Horizontal Backward Derailment under Continuous Gust;International Journal of Aerospace Engineering;2019-11-12

3. Computational Simulations of the Low-Noise SDT2-R4 Configuration Using Tenasi;2018 Applied Aerodynamics Conference;2018-06-24

4. Computational Simulations of a Multi-stage Subsonic Research Compressor;54th AIAA Aerospace Sciences Meeting;2016-01-02