Development of an aerodynamic simulation model of a generic configuration for S&C analyses
2014 (English)In: 32nd AIAA Applied Aerodynamics Conference, 2014Conference paper (Refereed)
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
IdentifiersURN: urn:nbn:se:kth:diva-168124ScopusID: 2-s2.0-84903885303OAI: oai:DiVA.org:kth-168124DiVA: diva2:815688
32nd AIAA Applied Aerodynamics Conference 2014; Atlanta, GA; United States
QC 201506012015-06-012015-05-272015-06-01Bibliographically approved