Over-wing integration of ultra-high bypass ratio engines: A coupled wing redesign and engine position study-Reference-Cited by-同舟云学术

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Over-wing integration of ultra-high bypass ratio engines: A coupled wing redesign and engine position study

Published:2023-07 Issue: Volume:138 Page:108350
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Tavares Silva Vinícius,Lundbladh Anders,Xisto Carlos^ORCID,Grönstedt Tomas^ORCID

Funder

Försvarsmakten

GKN Aerospace Services

Försvarets materielverk

VINNOVA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. A review of installation effects of ultra-high bypass ratio engines;Magrini;Prog. Aerosp. Sci.,2020

2. Aircraft engine technology for green aviation to reduce fuel burn;Hughes,2011

3. Powered low speed testing of the hybrid wing body;Wick,2017

4. Engine-over-the-wing noise research;Reshotko;J. Aircr.,1974

5. On noise assessment for blended wing body aircraft;Guo,2014

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1. Perception-based noise assessment of a future blended wing body aircraft concept using synthesized flyovers in an acoustic VR environment—The ARTEM study;Aerospace Science and Technology;2024-01

2. Powered Low-Speed Experimental Aerodynamic Investigation of an Over-Wing-Mounted Nacelle Configuration;Journal of Aircraft;2023-11-30

3. Comparison of Overwing and Underwing Nacelle Aeropropulsion Optimization for Subsonic Transport Aircraft;Journal of Aircraft;2023-09-05

4. Powered Low-speed Experimental Aerodynamic Investigation of an Over-wing Mounted Nacelle Configuration;AIAA AVIATION 2023 Forum;2023-06-08

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