Variable Bypass Ratio Engine Cycle Using Small Fan Devices
Dynamic Characteristic Tests of Single Spool Turbojet Engine Using Altitude Test Facility AIAA Paper
Simplified Analysis on Electromagnetic-Driving Fan for Aircraft Propulsion
Consideration on Gas Turbine Performance Improvement by an Advanced Cooling System
A user-friendly variation design method of free-form surfaces using a fundamental polyhedral shape
Electric Airbreathing Engine Concept for Future Airplanes