Fully Coupled Body Force–Engine Performance Methodology for Boundary Layer Ingestion-Reference-Cited by-同舟云学术

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Fully Coupled Body Force–Engine Performance Methodology for Boundary Layer Ingestion

Published:2021-03 Issue:2 Volume:37 Page:192-201
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

López de Vega Luis¹,Dufour Guillaume¹,García Rosa Nicolás¹

Affiliation:

1. University of Toulouse, 31055 Toulouse, France

Funder

Association Nationale de la Recherche et de la Technologie

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference28 articles.

1. Wake ingestion propulsion benefit

2. Power Balance in Aerodynamic Flows

3. Parametric Analysis and Design for Embedded Engine Inlets

4. Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft

5. Boundary Layer Ingestion Benefit of the D8 Transport Aircraft

Cited by 7 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. Body Force Modeling of the Fan Stage of a Windmilling Turbofan;Journal of Turbomachinery;2023-07-28

2. Extension and validation of the Body Force Method to a propeller blade;AIAA AVIATION 2023 Forum;2023-06-08

3. Advancements and prospects of boundary layer ingestion propulsion concepts;Progress in Aerospace Sciences;2023-04

4. Direct Software Coupling for Aeroplane Sizing and Integrated Aeroplane-Engine Mission Performance Simulations;AIAA SCITECH 2023 Forum;2023-01-19

5. Aeropropulsive assessment of engine installation at cruise for UHBPR turbofan with body force fan modelling;Aerospace Science and Technology;2023-01

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