Askin T. Isikveren
Askin T. Isikveren
Bauhaus Luftfahrt e.V.
Verified email at
Cited by
Cited by
Flight vehicle system identification: A time-domain methodology
RV Jategaonkar
American Institute of Aeronautics and Astronautics, Inc., 2015
Conceptual design of hybrid-electric transport aircraft
C Pornet, AT Isikveren
Progress in Aerospace Sciences 79, 114-135, 2015
Methodology for sizing and performance assessment of hybrid energy aircraft
C Pornet, C Gologan, PC Vratny, A Seitz, O Schmitz, AT Isikveren, ...
Journal of Aircraft 52 (1), 341-352, 2015
Conceptual studies of universally-electric systems architectures suitable for transport aircraft
AT Isikveren, A Seitz, PC Vratny, C Pornet, KO Plötner, M Hornung
Deutscher Luft-und Raumfahrt Kongress, 2012
Electrically powered propulsion: comparison and contrast to gas turbines
A Seitz, O Schmitz, AT Isikveren, M Hornung
Deutsche Gesellschaft für Luft-und Raumfahrt-Lilienthal-Oberth eV, 2012
Quasi-analytical modelling and optimisation techniques for transport aircraft design
AT Isikveren
Department of Aeronautics, 354, 2002
Pre-design strategies and sizing techniques for dual-energy aircraft
R Singh, AT Isikveren, S Kaiser, C Pornet, PC Vratny
Aircraft Engineering and Aerospace Technology: An International Journal, 2014
Morphing winglets for aircraft multi-phase improvement
N Ursache, T Melin, A Isikveren, M Friswell
7th AIAA ATIO Conf, 2nd CEIAT Int'l Conf on Innov and Integr in Aero …, 2007
Preliminary aerostructural optimization of a large business jet
P Piperni, M Abdo, F Kafyeke, AT Isikveren
Journal of Aircraft 44 (5), 1422-1438, 2007
Multi-disciplinary design and feasibility study of distributed propulsion systems
HJ Steiner, A Seitz, K Wieczorek, K Plötner, AT Isikveren, M Hornung
28th International Congress of the Aeronautical Sciences, 23-28, 2012
Progress and perspectives of electric air transport
H Kuhn, A Seitz, L Lorenz, AT Isikveren, A Sizmann
28th International Congress of the International Council of the Aeronautical …, 2012
Thermal buckling and vibration analysis of laminated composite curved shell panel
PV Katariya, SK Panda
Aircraft Engineering and Aerospace Technology: An International Journal, 2016
The Zigzag wingbox for a span morphing wing
RM Ajaj, EIS Flores, MI Friswell, G Allegri, BKS Woods, AT Isikveren, ...
Aerospace Science and Technology 28 (1), 364-375, 2013
Distributed propulsion and ultra-high by-pass rotor study at aircraft level
AT Isikveren, A Seitz, J Bijewitz, A Mirzoyan, A Isyanov, R Grenon, ...
The Aeronautical Journal 119 (1221), 1327-1376, 2015
Integrated fuel-battery hybrid for a narrow-body sized transport aircraft
R Singh, C Pornet, S Kaiser, AT Isikveren, M Hornung
Aircraft Engineering and Aerospace Technology: An International Journal, 2014
Small air transport aircraft entry requirements evoked by FlightPath 2050
K Piwek, W Wiśniowski
aircraft engineering and aerospace technology: an International Journal, 2016
Multi-objective optimization for the multiphase design of active polymorphing wings
DD Smith, RM Ajaj, AT Isikveren, MI Friswell
Journal of aircraft 49 (4), 1153-1160, 2012
A hybrid engine concept for multi-fuel blended wing body
AG Rao, F Yin, JP van Buijtenen
Aircraft Engineering and Aerospace Technology 86 (6), 483-493, 2014
Compliant structures-based wing and wingtip morphing devices
S Vasista, A De Gaspari, S Ricci, J Riemenschneider, HP Monner, ...
Aircraft Engineering and Aerospace Technology: An International Journal, 2016
Powder recyclability in electron beam melting for aeronautical use
VPR Niñerola
Aircraft Engineering and Aerospace Technology: An International Journal 87 …, 2015
The system can't perform the operation now. Try again later.
Articles 1–20