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journal of aerospace science and technology
سال:2005 - دوره:2 - شماره:1
A New Simple Analytical Model for Flow Analysis over Slender Delta Wings
- صفحه:15-19
A Two-Step Modification toward Implementing Compressible Source Terms in Low Compressible Flows
- صفحه:37-44
Effect of Electric Field on Liquid Viscosity in Co-Axial Cylindric Pipes
- صفحه:1-5
Material Characterization of Structures Using Genetic Algorithm and Viberational Data
- صفحه:21-27
On Efficiency of an Unstructured Grid Generation Method for Aerospace Applications
- صفحه:29-36
Three Dimensional Transonic Flow Computations Over a Projectile and at the Base Region
- صفحه:7-14
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