FLUID DYNAMICS - Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil
INTERDISCIPLINARY TOPICS - Reliability-Based Design Optimization of a Transonic Compressor
Multi-Objective Optimization of Transonic Compressor Blade Using Evolutionary Algorithm
Numerical Simulations of Membrane Wing Aerodynamics for Micro Air Vehicle Applications
INTERDISCIPLINARY TOPICS - Shape Optimization of a Membrane Wing for Micro Air Vehicles
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Membrane Wing Model for Micro Air Vehicles (TN)
Aerodynamics of Low Reynolds Number Plunging Airfoil in Gusty Environments
Numerical Investigation of Boundary Effects on Flapping Wing Study
Feature-Based Grid Adaption for the Study of Dynamic Stall (AIAA 2014-2997)
Investigation of Three-Dimensional Low Reynolds Number Tandem Flapping Wings
Numerical Study of Finite Aspect Ratio Perching Wings
A Framework for Interactions of Fluids and Rigid Bodies with Arbitrary Motions
Aerodynamic Response of Stationary and Flapping Wings in Oscillatory Low Reynolds Number Flows
Shape Optimization of a Membrane Wing for Micro Air Vehicles
The Effect of Wing Spacing on Tandem Wing Aerodynamics
Numerical Simulation of Supercooled Large Droplets Using the Moment of Fluid Method (AIAA 2014-0740)
Aerodynamics of Low Reynolds Number Plunging Airfoil Under Gusty Environment AIAA Paper
Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil
Investigation of Tip Vortex on Aerodynamic Performance of a Micro Air Vehicle
NUMERICAL STUDY OF TWO FLAPPING AIRFOILS IN TANDEM CONFIGURATION
Comparative Study of Pitch-Plunge Airfoil Aerodynamics at Transitional Reynolds Number
Three-Dimensional Fluid-Structure Interactions of a Membrane Wing for Micro Air Vehicle Applications
Numerical Investigation of the Aerodynamic and Structural Characteristics of a Corrugated Airfoil
RESUME OF THE AIAA FDTC LOW REYNOLDS NUMBER DISCUSSION GROUP'S CANONICAL CASES
Two-square target detection and imaging using NR-PC flat lens
The Study of Chemical Nonequilibrium Effect of Ablation on the Lifting Reentry Vehicles
AIAA 2006-0503 Flapping and Flexible Wing Aerodynamics of Low Reynolds Number Flight Vehicles
Development of a Parallel Hybrid Method for the DSMC and NS Solver
DESIGN OPTIMIZATION OF A VERTICAL AXIS WIND TURBINE USING A GENETIC ALGORITHM AND SURROGATE MODELS