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Aeroelastic analysis of the CAWAPI F-16XL configuration at transonic speeds
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Aerodynamics.
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2014 (English)In: 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, 2014Conference paper, Published paper (Refereed)
Abstract [en]

This article present an aeroelastic study of CAWAPI F-16XL aircraft. The structural model for this aircraft is publicly available and is therefore replaced by a structural model estimate which is constructed based on data available in public literature. The aeroelastic solution is done using inviscid solution for two flight conditions - FC70 and FC79. The primary task is to assess importance of the aeroelastic effects on the solution and to asses weather large discrepancies observed at flight condition FC70 between the computational and experimental data.

Place, publisher, year, edition, pages
2014.
Keyword [en]
Aerospace engineering, Aeroelastic analysis, Aeroelastic effects
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-168116Scopus ID: 2-s2.0-84902832288OAI: oai:DiVA.org:kth-168116DiVA: diva2:817025
Conference
Conference of 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
Note

QC 20150604

Available from: 2015-06-04 Created: 2015-05-27 Last updated: 2015-06-04Bibliographically approved

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