Journal of Aerospace Science and Technology

Boltzmann equation Development of a novel method in TRMC for a Binary Gas Flow Inside a Rotating Cylinder [Volume 5, Issue 2, 2008, Pages 67-79]
Boundary element method (BEM) Evaluation of 2-D Aeroelastic Models Based on Indicial Aerodynamic Theory and Vortex Lattice Method in Flutter and Gust Response Determination [Volume 5, Issue 4, 2008, Pages 180-182]
Boundary Layer Numerical Simulation of Separation Bubble on Elliptic Cylinders Using Three-equation k-? Turbulence Model [Volume 5, Issue 2, 2008, Pages 57-66]

Combined Loading Parametric Study of Plastic Load of Cylindrical Shells With Opening Subject to Combined Loading [Volume 5, Issue 2, 2008, Pages 91-98]
Composite plates- multiple delaminations- postbuckling- polynomial series Compressional Stability Behavior of Composite Plates with Multiple Through-the-Width Delaminations [Volume 5, Issue 1, 2008, Pages 13-22]
Critical flow Numerical Simulation of Separation Bubble on Elliptic Cylinders Using Three-equation k-? Turbulence Model [Volume 5, Issue 2, 2008, Pages 57-66]
Cylindrical Shell Parametric Study of Plastic Load of Cylindrical Shells With Opening Subject to Combined Loading [Volume 5, Issue 2, 2008, Pages 91-98]

DSMC Development of a novel method in TRMC for a Binary Gas Flow Inside a Rotating Cylinder [Volume 5, Issue 2, 2008, Pages 67-79]
Dynamic Response Evaluation of 2-D Aeroelastic Models Based on Indicial Aerodynamic Theory and Vortex Lattice Method in Flutter and Gust Response Determination [Volume 5, Issue 4, 2008, Pages 180-182]

Eddy-viscosity model Numerical Simulation of Separation Bubble on Elliptic Cylinders Using Three-equation k-? Turbulence Model [Volume 5, Issue 2, 2008, Pages 57-66]

Flapping wings – Unsteady Panel Method – Micro Aerial Vehicles NUMERICAL ANALYSIS OF MAVs FLAPPING WINGS IN UNSTEADY CONDITIONS [Volume 5, Issue 1, 2008, Pages 1-11]

Hardening models U-Bending Analysis with an Emphasis on Influence of Hardening Models [Volume 5, Issue 1, 2008, Pages 45-50]

Indicial aerodynamic theory Evaluation of 2-D Aeroelastic Models Based on Indicial Aerodynamic Theory and Vortex Lattice Method in Flutter and Gust Response Determination [Volume 5, Issue 4, 2008, Pages 180-182]

Laminar separation bubble Numerical Simulation of Separation Bubble on Elliptic Cylinders Using Three-equation k-? Turbulence Model [Volume 5, Issue 2, 2008, Pages 57-66]
Limit Load Parametric Study of Plastic Load of Cylindrical Shells With Opening Subject to Combined Loading [Volume 5, Issue 2, 2008, Pages 91-98]

Plastic Analysis Parametric Study of Plastic Load of Cylindrical Shells With Opening Subject to Combined Loading [Volume 5, Issue 2, 2008, Pages 91-98]
Poincare map Preload Effect on Nonlinear Dynamic Behavior of Aerodynamic Two-Lobe Journal Bearings [Volume 5, Issue 4, 2008, Pages 145-159]
Preload Preload Effect on Nonlinear Dynamic Behavior of Aerodynamic Two-Lobe Journal Bearings [Volume 5, Issue 4, 2008, Pages 145-159]

Recognition-Visual Identification-Neural Networks-Image Processing Aircraft Visual Identification by Neural Networks [Volume 5, Issue 3, 2008, Pages 123-128]

Sharp edge gust Evaluation of 2-D Aeroelastic Models Based on Indicial Aerodynamic Theory and Vortex Lattice Method in Flutter and Gust Response Determination [Volume 5, Issue 4, 2008, Pages 180-182]
Solid state wave gyroscope Analysis of a solid state wave gyroscope with thin shell cylindrical resonator and calculation of its conversion factor [Volume 5, Issue 4, 2008, Pages 167-174]
Springback U-Bending Analysis with an Emphasis on Influence of Hardening Models [Volume 5, Issue 1, 2008, Pages 45-50]

Tow-lobe bearing Preload Effect on Nonlinear Dynamic Behavior of Aerodynamic Two-Lobe Journal Bearings [Volume 5, Issue 4, 2008, Pages 145-159]
TRMC Development of a novel method in TRMC for a Binary Gas Flow Inside a Rotating Cylinder [Volume 5, Issue 2, 2008, Pages 67-79]

U-bending U-Bending Analysis with an Emphasis on Influence of Hardening Models [Volume 5, Issue 1, 2008, Pages 45-50]

Vortex lattice method (VLM) Evaluation of 2-D Aeroelastic Models Based on Indicial Aerodynamic Theory and Vortex Lattice Method in Flutter and Gust Response Determination [Volume 5, Issue 4, 2008, Pages 180-182]