Axial Compressor Design

Axial Compressor Design is the engineering methodology concerned with the systematic development and optimization of axial-flow compressors for gas turbine propulsion systems, distinguished by its focus on aerodynamic profiling, stage stacking, and performance prediction to achieve desired pressure rise, efficiency, and operational stability.

390

Publications

11.8K

Citations

834

Authors

227

Institutions

Publications per year

2017–2026

Parents

Gas Turbine Propulsion

Publications

390

Multiple Surrogate Modeling for Axial Compressor Blade Shape Optimization

Abdus Samad, Kwang‐Yong Kim, Tushar Goel et al. · Journal of Propulsion and Power · 2008 · 210 citations

Architecture, Aerospace Engineering, Mechanical Engineering +17

A Criterion for Axial Compressor Hub-Corner Stall

Vai-Man Lei, Z. S. Spakovszky, E. M. Greitzer · Journal of Turbomachinery · 2008 · 207 citations

Engineering, Aerospace Engineering, Computational Engineering +13

Endwall Blockage in Axial Compressors

S. Arif Khalid, Amrit S. Khalsa, Ian A. Waitz et al. · Journal of Turbomachinery · 1999 · 180 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14

The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading—Part I: University Research and Methods Development

S. J. Gallimore, John J. Bolger, N. A. Cumpsty et al. · Journal of Turbomachinery · 2002 · 166 citations

Engineering, Aerospace Engineering, Mechanical Engineering +16

Streamline Curvature Computing Procedures for Fluid-Flow Problems

Richard A. Novak · Journal of Engineering for Power · 1967 · 161 citations

Engineering, Aerospace Engineering, Mechanical Engineering +11

1–5 of 390

Authors

834

KK
Kwang‐Yong Kim
Inha University, South Korea
12 publications · 574 citations
12
h-index
NA
N. A. Cumpsty
University of Cambridge, United Kingdom
9 publications · 761 citations
9
h-index
EN
Eberhard Nicke
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
8 publications · 273 citations
8
h-index
AH
Alexander Hergt
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
7 publications · 219 citations
7
h-index
XM
Xiaochen Mao
Northwestern Polytechnical University, China
7 publications · 184 citations
7
h-index

1–5 of 834

Institutions

227

1–8 of 227

Venues

Journal of Turbomachinery
59 publications · 2.7K citations
29
h-index
Aerospace Science and Technology
AST · 38 publications · 1.1K citations
22
h-index
Journal of Thermal Science
11 publications · 196 citations
11
h-index
Volume 1: Turbomachinery
Conference · 11 publications · 293 citations
11
h-index
Journal of Engineering for Gas Turbines and Power
11 publications · 370 citations
11
h-index

1–5