Change search
ReferencesLink to record
Permanent link

Direct link
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 (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
National Category
Aerospace Engineering
URN: urn:nbn:se:kth:diva-168124ScopusID: 2-s2.0-84903885303OAI: diva2:815688
32nd AIAA Applied Aerodynamics Conference 2014; Atlanta, GA; United States

QC 20150601

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

Open Access in DiVA

No full text


Search in DiVA

By author/editor
Rizzi, Arthur
By organisation
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 29 hits
ReferencesLink to record
Permanent link

Direct link