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journal of aerospace science and technology
سال:2012 - دوره:9 - شماره:1
A Comprehensive Approach to Develop a Continuous Fuzzy Guidance Law for Maneuvering Targets
- صفحه:27-36
An Innovation in Film Cooling of Gas Turbine Blades Applying an Upstream Jet
- صفحه:13-26
Crack Analysis, Using a New Coupled FE-EFG Method
- صفحه:59-73
Effect of Wing Sweep Angle on The Vortex Interaction of a Tail-Wing Configuration
- صفحه:1-11
Helicopter Rotor Airloads Prediction, Using CFD and Flight Test Measurement in Hover Flight
- صفحه:37-48
Performance Modeling and Examination of Losses in the Axial -Flow Compressor
- صفحه:75-86
Practical Evaluation of EKF^1 and UKF^2 Filters for Terrain Aided Navigation
- صفحه:49-58
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