Flugwissenschaftliche Vereinigung Aachen is a non-profit organization, founded in 1920, which is closely associated to RWTH Aachen University, with members consisting ofRWTH Aachen students, which have included Felix Kracht. FVA supports and organizes various training courses for flight training, handling of composites and other aircraft materials including steel and aluminum. Projects handled include research into alternative flaps configuration for Airbus aircraft. As a reward for work carried out in the laboratories and workshops at FVA, 300 hours per annum minimum, each student is granted free flying at the FVA gliding club. Training at the gliding club includes flying gliders, and glider tugs as well as flying instructor training, workshop supervisors and parachute packers. The FVA is under the wing of IDAFLIEG and takes part in the Summer and Winter camps and seminars organised by IDAFLIEG. Through designing, constructing and flight testing of aircraft and research projects the students can complete their studies, publishing results and theses and gaining valuable skills knowledge and experience. The glider fleet at FVA Aachen includes a high performance two-seat DG-1000 training glider, Schleicher ASH 25E open class two-seater, Glasflügel 205 Club Libelle and Glasflügel 206 Hornetclub class gliders, as well as a Schleicher ASW 28-18 18m class sailplane, all of which can be flown by suitably qualified students. A Robin DR400 for towing the sailplanes is also owned by the FVA.
Projects
The FVA has undertaken the following development projects: ;FVA-1 Schwatze Düvel ;FVA-2 Blaue Maus ;FVA-3 Ente ;FVA-4 Pipö ;FVA-5 Rheinland ;FVA-6 ;FVA-7 M Ia ;FVA-8 MS II ;FVA-9 Blaue Maus II ;FVA-10a Theodor Bienen ;FVA-10b Rheinland ;FVA-11 Eifel ;FVA-12 ;FVA-13 Olympia-Jolle ;FVA-14 Ringflügel ;FVA-15 ;FVA-16 Schaumstoff-Flügel ;FVA-17 Nurflügler ;FVA-18 Primitiv Krähe ;FVA-19 Silberkrähe ;FVA-20 ;FVA-21 Wölbklappenautomatik ;FVA-22 Papierrakete ;FVA-23 ;FVA-24 Wimi ;FVA-27 The anticipated improvements/advantages include:
Increased aspect ratio through reduced area, while retaining 15m span.
Reduced drag through reduction in fuselage wetted area.
