B
-
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]
C
-
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]
D
-
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]
E
-
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]
F
-
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]
H
-
Hardening models
U-Bending Analysis with an Emphasis on Influence of Hardening Models [Volume 5, Issue 1, 2008, Pages 45-50]
I
-
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]
L
-
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]
P
-
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]
R
-
Recognition-Visual Identification-Neural Networks-Image Processing
Aircraft Visual Identification by Neural Networks [Volume 5, Issue 3, 2008, Pages 123-128]
S
-
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]
T
-
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
-
U-bending
U-Bending Analysis with an Emphasis on Influence of Hardening Models [Volume 5, Issue 1, 2008, Pages 45-50]
V
-
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]