Abgasanalyse mit ibm system 1800
Aerodynamic Optimal Engine Integration at the Fuselage Tail of a Generic Business Jet Configuration
Blended wing body lateral-directional stability investigation using 6DOF simulation
Efficient approach for multipoint aerodynamic wing design of business jet aircraft
Parallel implementation of fictitious surfaces method for aerodynamic shape optimization
Primer Coating; Epoxy, Chemical and Solvent Resistant Non-Chromated, Corrosion Preventive