شماره 1 تاریخ انتشار 2633-04-21

• Effect of Wing Sweep Angle on the Vortex Interaction of a Tail-Wing Configuration
• An Innovation in Film Cooling of the Gas Turbine Blades Applying an Upstream Jet
• A Comprehensive Approach to Develop a Continuous Fuzzy Guidance Law for Maneuvering Targets
• Helicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight
• Practical Evaluation of EKF1 and UKF2 Filters for Terrain Aided Navigation
• Performance Modeling and Examination of Losses in the Axial -Flow Compressor and Comparisonwith Experimental Results
• Crack Analysis, Using a New Coupled FE-EFG Method