CFD analysis of wing-propeller interaction on the NASA X-57 Maxwell aircraft wing
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F24%3APU151434" target="_blank" >RIV/00216305:26210/24:PU151434 - isvavai.cz</a>
Result on the web
<a href="https://iopscience.iop.org/article/10.1088/1742-6596/2716/1/012002/meta" target="_blank" >https://iopscience.iop.org/article/10.1088/1742-6596/2716/1/012002/meta</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1088/1742-6596/2716/1/012002" target="_blank" >10.1088/1742-6596/2716/1/012002</a>
Alternative languages
Result language
angličtina
Original language name
CFD analysis of wing-propeller interaction on the NASA X-57 Maxwell aircraft wing
Original language description
Due to global warming concerns, the Aviation industry is trying to reduce its carbon footprint. Electric propulsion (EP) is one way of doing this, where the power is obtained from electrical sources. The concept of distributed electric propulsion (DEP) is in the focus now. NASA's X-57 Maxwell, a high winged, all-electric experimental aircraft, uses this concept. The present work aims at developing a CFD model (ANSYS Fluent) to evaluate aerodynamic performance of two configurations of NASA's X-57 aircraft wing; (i) wing and nacelle (clean wing) and (ii) wing, nacelle and one electric propeller under cruise condition; and compare it with the results of wind tunnel experiment performed by NASA/Armstrong X-57 research program. Parameters like lift, drag and pressure coefficients (CL, CD, CP) are compared for both cases. A good match is observed for CL, CD and CP, thus validating the model. The unsteady RANS solver is very efficient in capturing the effects of propeller slipstream on the wing. After validation, this model is further used to simulate aerodynamic performance of a wing with multi-propeller (DEP) configuration. © Published under licence by IOP Publishing Ltd.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2024
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons
ISBN
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ISSN
1742-6588
e-ISSN
1742-6596
Number of pages
8
Pages from-to
1-8
Publisher name
IOP Publishing
Place of publication
neuveden
Event location
Salerno
Event date
Sep 5, 2023
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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