ISSN: 0334-0082

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International Journal of Turbo and Jet Engines Q3 Unclaimed

Walter de Gruyter GmbH Germany

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International Journal of Turbo and Jet Engines is a journal indexed in SJR in Aerospace Engineering with an H index of 27. It has an SJR impact factor of 0,279 and it has a best quartile of Q3. It is published in English. It has an SJR impact factor of 0,279.

Type: Journal

Type of Copyright:

Languages: English

Open Access Policy:

Type of publications:

Publication frecuency: -

Categories: Aerospace Engineering (Q3)

Price

- €

Inmediate OA

NPD

Embargoed OA

- €

Non OA

Metrics

International Journal of Turbo and Jet Engines

0,279

SJR Impact factor

27

H Index

131

Total Docs (Last Year)

181

Total Docs (3 years)

3397

Total Refs

207

Total Cites (3 years)

181

Citable Docs (3 years)

1.01

Cites/Doc (2 years)

25.93

Ref/Doc

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering Q3
International Journal of Micro Air Vehicles Q3
Yuhang Xuebao/Journal of Astronautics Q3
International Journal of Aerospace Engineering Q3

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Aims and Scope

Best articles by citations

Global Needs for Jet-Engine-Steered (JES) Strike Drones vs. Lack of Updated Textbooks to Design 6th Generation UCLASS Due to UCAV Failure

Fatigue Life Prediction of Fan Blade Using Nominal Stress Method and Cumulative Fatigue Damage Theory

Influence of 3D Hot Streaks on Turbine Heat Transfer

Probabilistic Fatigue Life Prediction of Turbine Disc Considering Model Parameter Uncertainty

Frequency-domain Model Matching PID Controller Design for Aero-engine

Editorial on Future Jet Technologies

Engine Life Maturation Process

Study of the Standard k-e Model for Tip Leakage Flow in an Axial Compressor Rotor

Assessment Of Navier-Stokes and Boundary Layeer Procedures for the Prediction of Two-Dimensional Viscous Flow in a Turbine Nozzle

Lightweight Magnesium Bipolar Plates of Direct NaBH4/H2O2 Fuel Cell for AIP Application

Effect of Axial Velocity Density Ratio on the Performance of a Controlled Diffusion Airfoil Compressor Cascade

CFD Modeling of Mixed-Phase Icing

SHOW MORE ARTICLES

Frequency Domain Identification of Multivariable Model for Aero-Engine using an Improved Maximum Likelihood Method

Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer

Predicting Lean Blowout and Emissions of Aircraft Engine Combustion Chamber Based on CRN

Research on Inverse, Hybrid and Optimization Problems in Engineering Sciences with Emphasis on Turbomachine Aerodynamics: A Review of Chinese Advances

Tab Aspect Ratio Effect on Supersonic Jet Mixing

Large Eddy Simulation of Secondary Flows in an Ultra-High Lift Low Pressure Turbine Cascade at Various Inlet Incidences

Full-Range Mathematical Modeling of Turboshaft Engine in Aerospace

CFD Study of Combined Impingement and Film Cooling Flow on the Internal Surface Temperature Distribution of a Vane

Variable-Domain Finite Element Method Based on Variational Principles for Solving Hybrid Problems of Fully 3-D Compressible Rotor-Flow

Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model

Investigation of Flow Distortion Generated Forced Response of a Radial Turbine with Vaneless Volute

Tensile Behavior and Microstructural Evolution of the Polycrystalline Nickel-Based Superalloy Applied in Turbine Disk