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Development of an aerodynamic simulation model of a generic configuration for S&C analyses
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Aerodynamics.
2014 (English)In: 32nd AIAA Applied Aerodynamics Conference, 2014Conference paper, Published paper (Refereed)
Abstract [en]

The development of an aerodynamic simulation model for the inclusion in an open-loop Stability & Control model is presented. The model, based on a generic UCAV configuration, is derived from data gathered during a number of experimental campaigns conducted using various test models and facilities, and covers the full subsonic flight regime. The model includes uncertainties in key model parameters to yield an expected range of model outputs for any given condition.

Place, publisher, year, edition, pages
2014.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-168124Scopus ID: 2-s2.0-84903885303OAI: oai:DiVA.org:kth-168124DiVA: diva2:815688
Conference
32nd AIAA Applied Aerodynamics Conference 2014; Atlanta, GA; United States
Note

QC 20150601

Available from: 2015-06-01 Created: 2015-05-27 Last updated: 2015-06-01Bibliographically approved

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CiteExportLink to record
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