A TIME ACCURATE ZONAL FINITE ELEMENT METHOD FOR SOLVING COMPRESSIBLE AND INCOMPRESSIBLE VISCOUS FLOWS
INTEGRATED AIRCRAFT ENGINE DESIGN-THE IMPLEMENTATION OF THE MASTER MODEL CONCEPT AT GE AIRCRAFT ENGINES
THE ZERO SPLICE ENGINE INTAKE LINER:AN EFFICIENT WAY OF REDUCING AIRCRAFT NOISE WITHOUT ANY WEIGHT OR AERODYNAMIC PENALTY.
STRUCTURAL LOADING OF A COMPLETE AIRCRAFT UNDER REALISTIC CRASH CONDITIONS: GENERATION OF A LOAD DATABASE FOR PASSENGER SAFETY AND INNOVATIVE DESIGN
Application of Pressure-Sensitive Paint to Low-Speed Wind Tunnel Testing at Japan Aerospace Exploration Agency