Advanced Mach 3.5 Axisymmetric Quiet Nozzle

Author:

CHEN FANG-JENQ1,MALIK MUJEEB1,BECKWITH IVAN2

Affiliation:

1. High Technology Corp., Hampton, VA

2. NASA, Langley Research Center; George WashingtonUniversity, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Boundary-layer instability measurements on a cone at freestream Mach 3.5;Physics of Fluids;2021-10

2. 40 Years of Transition Research at NASA: A Personal Perspective;IUTAM Laminar-Turbulent Transition;2021-07-31

3. Measurements in a Transitioning Cone Boundary Layer at Freestream Mach 3.5;54th AIAA Aerospace Sciences Meeting;2016-01-02

4. Off-Body Boundary-Layer Measurement Techniques Development for Supersonic Low-Disturbance Flows;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

5. High-Speed Boundary-Layer Transition Induced by an Isolated Roughness Element;40th Fluid Dynamics Conference and Exhibit;2010-06-28

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