An integrated review of multiphysics issues and challenges in the design and implementation of gas turbine blades for jet engine applications

Abstract Gas turbine blades are critical components subjected to extreme operating conditions, where the relentless demand for higher efficiency and durability drives innovation. This paper provides a critical review of recent advancements in turbine blade engineering, identify key challenges, and illuminate future directions. The review navigates the intricate relationship between six interconnected pillars: aerodynamic design, materials engineering, thermal management, structural analysis, life prediction, and the impact of advanced manufacturing. Despite significant progress in computational modeling, this review highlights a persistent and consequential reality gap between idealized predictions and the performance of in-service hardware. This gap is driven by factors such as manufacturing imperfections, environmental degradation, cooling effectiveness decay, and the process-induced defects inherent to novel technologies like additive manufacturing. Closing this gap is identified as the single most significant challenge, requiring a rigorous fusion of predictive modeling with comprehensive validation against data from service-exposed components.

Authors

Institutions

Publication Details

Journal
International Journal of Turbo and Jet Engines
Published
2025-12-26
DOI
https://doi.org/10.1515/tjj-2025-0104
Primary Topic
High Temperature Alloys and Creep
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

An integrated review of multiphysics issues and challenges in the design and implementation of gas turbine blades for jet engine applications

Raja Sekhar Dondapati, Akash Pawar
International Journal of Turbo and Jet Engines
High Temperature Alloys and Creep
article

An integrated review of multiphysics issues and challenges in the design and implementation of gas turbine blades for jet engine applications

Raja Sekhar Dondapati, Akash Pawar
article en

Abstract

Abstract Gas turbine blades are critical components subjected to extreme operating conditions, where the relentless demand for higher efficiency and durability drives innovation. This paper provides a critical review of recent advancements in turbine blade engineering, identify key challenges, and illuminate future directions. The review navigates the intricate relationship between six interconnected pillars: aerodynamic design, materials engineering, thermal management, structural analysis, life prediction, and the impact of advanced manufacturing. Despite significant progress in computational modeling, this review highlights a persistent and consequential reality gap between idealized predictions and the performance of in-service hardware. This gap is driven by factors such as manufacturing imperfections, environmental degradation, cooling effectiveness decay, and the process-induced defects inherent to novel technologies like additive manufacturing. Closing this gap is identified as the single most significant challenge, requiring a rigorous fusion of predictive modeling with comprehensive validation against data from service-exposed components.

International Journal of Turbo and Jet Engines
Lovely Professional University (IN)
Responsible consumption and production
Openalex Percentile: Top 44%
High Temperature Alloys and Creep
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

An integrated review of multiphysics issues and challenges in the design and implementation of gas turbine blades for jet engine applications — Raja Sekhar Dondapati, Akash Pawar · International Journal of Turbo and Jet Engines (2025) | TGRS Research Map | TGRS