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Investigation of Air Tab's Effect in Supersonic Jets

  • Published:2011-09 Issue:5 Volume:27 Page:1157-1160
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

Wan C.1,Yu S.C.M.1

Affiliation:

1. Nanyang Technological University, Singapore 639798, Republic of Singapore

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Cited by 20 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. Role of strut shape on the generation of internal side force and moments in A supersonic nozzle with strut insertion through diverging wall;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-07-17

2. Rectangular Sonic Jet Control with Supersonic Fluidic Injectors;Journal of Aerospace Engineering;2024-05

3. Air tab location effect on supersonic jet mixing;International Journal of Turbo & Jet-Engines;2024-04-04

4. An experimental study on supersonic jet control using shifted air tabs;Journal of Thermal Engineering;2024

5. Study of wedge-shaped Jet tabs for effective Thrust vector control in Supersonic vehicles;Aerospace Systems;2023-12-08
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