Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring-Reference-Cited by-同舟云学术

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Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring

Published:2016-07-22 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
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Author:

Ferlauto Michele,Marsilio Roberto

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4504

Reference31 articles.

1. High-alpha vectoring characteristics of the F-18/HARV

2. Aircraft Control Using Fluidic Maneuver Effectors

3. Fluidic Thrust Vectoring for Low Observable Air Vehicles

4. Summary of Fluidic Thrust Vectoring Research at NASA Langley Research Center

Cited by 7 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. A Framework for Testing Differential Throttling in Linear Aerospike Nozzle;2024 11th International Workshop on Metrology for AeroSpace (MetroAeroSpace);2024-06-03

2. Dynamic characteristics and application of dual throat fluidic thrust vectoring nozzle;Chinese Journal of Aeronautics;2024-04

3. Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle;AIAA SCITECH 2024 Forum;2024-01-04

4. Influence of Hot Flow Conditions on Nozzle Performances;AIAA SCITECH 2023 Forum;2023-01-19

5. Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring;AIAA AVIATION 2022 Forum;2022-06-20

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