DEVELOPMENT OF THE PRESSURE-SENSITIVE PAINT MEASUREMENT FOR LARGE WIND TUNNELS AT JAPAN AEROSPACE EXPLORATION AGENCY
THE AIRBUS/ENGINE & NACELLE MANUFACTURERS RELATIONSHIP:TOWARS A MORE INTEGRATED, ENVIRONMENTALLY FRIENDLY ENGINEERING DESIGN
NATURAL FREQUENCIES OF ROTATING CANTILEVER FLEXIBLE BEAMS BY USING THE p-VERSION OF THE FINITE ELEMENT METHOD
INFLUENCE OF THE STORE ON THE TRANSONIC AND SUPERSONIC FLUTTER CHARACTERISTICS OF A DELTA WING CONFIGURATION