REDUCING ICING CERTIFICATION FLIGHT TESTS THROUGH SECOND-GENERATION 3-D CFD-BASED TECHNOLOGIES
Navier-Stokes Computations of Fuselage Drag Increments
Navier-Stokes Computations of Fuselage Drag Increments
Navier-Stokes Computation of Unsteady Internal Airloads
Navier-Stokes Computation of Unsteady Internal Airloads
FENSAP-ICE: Progress Towards a Rotorcraft Full 3-D Icing Simulation System
FENSAP-ICE Applications to Complete Rotorcraft Configurations
Design and Evaluation of Multi-Element Airfoils for Rotorcraft
Computational Fluid Dynamics Development and Validation at Bell Helicopter
Application of Computational Fluid Dynamics to the Design of the 916 Deepwater UAV
An Approach to Subsonic, Turbulent Flow Airfoil Design Using Mini-Computers
Advanced Parallel Computing Systems Application to the V-22 TiltRotor
Actuator Disk Implementation in FENSAP-ICE, a 3D Navier-Stokes In-Flight Icing Simulation System