Improvement of Wide-Chord Rotor Blade Fan Performance in Bypass Turbojet Engine

Herald of Aeroenginebuilding
doi 10.15588/1727-0219-2018-1-6
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Zaporizhzhia National Technical University

Related search

Turbojet and Turbofan Engine Performance Increases Through Turbine Burners

Journal of Propulsion and Power
SpacePlanetary ScienceFuel TechnologyMechanical EngineeringAerospace Engineering
2001English

Evaluation of Ceiling Fan Blade Angle Performance Using CFD

International Journal of Trend in Scientific Research and Development
2018English

Modelling of Vane and Rotor Blade Rows in Simulations of Gas Turbine Performance

Journal of KONES
2019English

A Detailed Procedure for Measuring Turbojet Engine Performance in an Enclosed Sea-Level Test Facility.

English

Rotordynamic Analysis of Asymmetric Turbofan Rotor Due to Fan Blade-Loss Event With Contact-Impact Rub Loads

Journal of Sound and Vibration
Mechanics of MaterialsAcousticsUltrasonicsCondensed Matter PhysicsMechanical Engineering
2013English

Experiment Modeling Under Impact of Torn Vane With Turbojet Fan Case

Perm National Research Polytechnic University Aerospace Engineering Bulletin
2018English

Performance Evaluation of a Small-Scale Turbojet Engine Running on Palm Oil Biodiesel Blends

Journal of Fuels
2014English

The Effect Variation Arch of Rotor Blade on the Performance of Kinetic Turbine

2019English

Optical Measurement of Unducted Fan Blade Deflections

Journal of Turbomachinery
Mechanical Engineering
1990English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy