Aircraft Design, Testing and Performance

Related articles 11 - 20 of 82
First page Previous page Page 2 of 9 Next page Last page

Integrated Aircraft Design


The performance of aircraft is not equivalent to flight performance only but to the aircrafts impact on the efficiency of the entire transportation chain. Thus; the simulation of the transportation sy...
http://www.dlr.de/lk/en/desktopdefault.aspx/tabid-4463/7268_read-10956/
Related Topics: Aircraft Design, Testing and Performance

Air Transportation Systems


DLR Air Transportation Systems stands for research and teachings on the understanding of the system complexities in air transport. The research portfolio comprises of concepts, preliminary designs an...
http://www.dlr.de/lk/en/desktopdefault.aspx/tabid-4449/7262_read-47289/
Related Topics: Research and Support Facilities (Air) Aircraft Design, Testing and Performance Air Transportation and Safety

2nd Annual Project Workshop MEGADESIGN


The German national project MEGADESIGN and the complementary DLR project MegaOpt deal with "Aerodynamic Simulation and Optimization in Aircraft Design". The current status of work and related results ...
http://www.dlr.de/as/en/desktopdefault.aspx/tabid-396/530_read-2205/
Related Topics: Aircraft Design, Testing and Performance

Flight Facility Braunschweig


The DLR Flight Facility Braunschweig is a major test site for aerodynamic research, in-flight simulation and testing of flight management, air traffic management and remote sensing systems. It operate...
http://www.dlr.de/fb/en/desktopdefault.aspx/tabid-3686/5733_read-8351/
Related Topics: Aircraft Design, Testing and Performance

Unsteady Aerodynamic Modelling


The knowledge of unsteady aerodynamic loads acting on an aircraft structure, which is moving either uniformly (steady) or accelerated (manoeuvring or oscillating), or within an unsteady environment (a...
http://www.dlr.de/ae/en/desktopdefault.aspx/tabid-4120/6539_read-9287/
Related Topics: Aerodynamic Aircraft Design, Testing and Performance

iDEAL - inverse Design for Early Aicraft Layout


Goal of the internal department project iDEAL (inverse Design for Early Aircraft Layout) is the development and demonstration of new processes and methods for a fast identification of the global desig...
http://www.dlr.de/ft/en/desktopdefault.aspx/tabid-1360/1856_read-43457/
Related Topics: Aircraft Stability and Control Aircraft Design, Testing and Performance

ATTAS


The flight test bed VFW614/ATTAS is based on the two engine, short haul, 44-seats passenger jet VFW614, which was developed and built in the seventies in Bremen/Germany by the VFW-Fokker company (toda...
http://www.dlr.de/fb/en/desktopdefault.aspx/tabid-3707/5786_read-8393/
Related Topics: Aircraft Stability and Control Aircraft Design, Testing and Performance Avionics and Aircraft Instrumentation

FrEACs - Future Enhanced Aircraft Configurations


The Department Safety Crticial Systems and Systems Engineering (SSY) is responsible for the design of the flight control system for the BWB configuration. The data format Premise, developed by the dep...
http://www.dlr.de/ft/en/desktopdefault.aspx/tabid-1360/1856_read-45380/
Related Topics: Aircraft Design, Testing and Performance
First page Previous page Next page Last page