Abgasturboladerkonzepte fur heutige und zukunftige Nutzfahrzeugmotoren
A Dynamic Load Distribution Method for a Usage Spectrum Fatigue Test of a Fighter Aircraft Wing
Appendix E — Comparison of the improved Di Giovanni/Radicella model
Appendix E - Comparison of the Improved Di Giovanni-Radicella Model
Assessment of two fluidic actuators for active flow control on a one-sided diffuser
Assessment of two fluidic actuators for active flow control on a one-sided diffuser
Creative Team Solutions - without Frontiers - Telecooperation in Chassis and Suspension Development
Development and Validation of an Aircraft Multipath Model for Land-Based JPALS
Development of Versatile Polymer Waveguide Flex Technology for Use in Optical Interconnects
Direct Jack Optimization for the Loading of the Wing by the Swiss F/A-18 Full Scale Fatigue Test
Effects of Low-Amplitude Cycles in Spectrum Loading on a Fighter Aircraft
Evaluation of a Thermal-Tuft Probe for Turbulent Separating and Reattaching Flows (AIAA 2014-1242)
Fiber optic strain and temperature sensors for power plant applications [2594-16]