Design and Evaluation of Aeroelastically Tuned Joined-Wing SensorCraft Flight Test Article
Design and Evaluation of Aeroelastically Tuned Joined-Wing SensorCraft Flight Test Article
Steuersystem zum Beurteilen eines Bremskraftverstärkersystems
Numerical Rate Equation Modeling of a ∼ 2.1 - μm - Tm^3^+/Ho^3^+ Co-Doped Tellurite Fiber Laser