Comparison of Rocket Near-Wakes with and without Nozzle Simulation in Subsonic Freestream Conditions

Author:

Wolf Christian1,Klei Christine1,Buffo Rainer1,Hörnschemeyer Ralf1,Stumpf Eike1

Affiliation:

1. RWTH Aachen University

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. Coherent motions in a turbulent wake of an axisymmetric bluff body;Journal of Fluid Mechanics;2023-04-28

2. Future Developments of Light-field-Based Measurements;Development and Application of Light-Field Cameras in Fluid Measurements;2022-08-14

3. Experimental study of the boosters impact on the rocket aerodynamic characteristics;Aircraft Engineering and Aerospace Technology;2022-07-21

4. Effects of Exhaust Plume and Nozzle Length on Compressible Base Flows;AIAA Journal;2019-03

5. Afterbody Effects on Axisymmetric Base Flows;AIAA Journal;2016-08

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