1. Vicroy, D.D., Huber, K.C., Löser, T., Rohlf, D.: “Low-speed dynamic wind tunnel test analysis of a generic 53° swept UCAV configuration with controls”, 32nd AIAA applied aerodynamics conference, AIAA-2014-2003. Atlanta, GA (2014)
2. Schütte, A., Huber, K.C., Zimper, D.: “Numerische Aerodynamische Analyse und Bewertung einer agilen hoch gepfeilten Flugzeugkonfiguration,” Deutscher Luft- und Raumfahrtkongress, Rostock, 22–24 Sep 2015
3. Cummings, R.M., Schütte, A. et al.: “Assessment of stability and control prediction methods for nato air and sea vehicles,” NATO RTO/AVT, final report of the AVT-161 task group, RTO-TR-AVT-161, September 2012
4. Huber, K. C., Schütte, A., Rein, M.: “Numerical investigation of the aerodynamic properties of a flying wing configuration,” 30th AIAA Applied Aerodynamics Conference, AIAA -2012-3325, 2012
5. Schütte, A., Hummel, D., Hitzel, S.M.: Flow physics analyses of a generic unmanned combat aerial vehicle configuration. J. Aircr. 49(6), 1638–1651 (2012)