1. Optimum Subsonic, High-Angle-Of-Attack Nacelles;Luidens,1980
2. Ultrashort nacelles for low fan pressure ratio propulsors;Peters;ASME Journal of Turbomachinery,2015
3. Flow control opportunities in gas turbine engines;Lord,2000
4. Intake engine interactions of a modern large turbofan engine;Freeman,1999
5. The history of boundary layer control research in the United States of America;Flatt,1961