Multi-Block Grid Generation for Complete Aircraft Configurations
Laminar-Turbulent Transition Process in the Presence of Simulated Wall Roughness
Aircraft Take-Off Laboratory Simulation for De/Anti-Icing Study
A Scheme for Two-Dimensional Euler and Boundary-Layer Interactive Solutions
A Convenient Airborne Mil-STD-1553 Multiplex Data Bus Data Acquisition System
Off-Design Performance Prediction of Turbofans Using Gas Dynamics
Development of a Transonic Euler Method for Complete Aircraft Configurations