Mohammed Khalil Ibrahim
Professor and Head of Aerodynamics Group
Faculty of Engineering, Aerospace Engineering Department, Cairo University, Giza 12613, Egypt (email)
Effects of Rotating Tabs on Flow and Acoustic Fields of Supersonic Jet
- Citation:
- IBRAHIM, M. K., and Y. Nakamura, "Effects of Rotating Tabs on Flow and Acoustic Fields of Supersonic Jet", AIAA Journal, vol. 39, issue 4, pp. 745-748, 2002. copy at www.tinyurl.com/z4akkz9