Influence of secondary injection parameters on performance of shock vector control nozzle
Author:
Affiliation:
1. China Aerodynamics Research and Development Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2270
Reference21 articles.
1. Deere K A., Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley ResearchCenter[R].AIAA-2003-3800,2003.
2. Chiarelli, C. Johnsen, R. K. Shieh, C. F. Wing, D. J. Fluidic Scale Model Multi-Plane Thrust VectorControlTestResults[R].AIAA-1993-2433,June1993.
3. Wing, David J. Static Investigation of Two Fluidic Thrust-Vectoring Concepts on a Two-DimensionalConvergent-DivergentNozzle[R].NASATM-4574,December1994.
4. Deere K.A., PAB3D Simulations of a Nozzle With Wluidic Injection for Yaw Thrust-Vector Control[R],AIAA98-3254,1998.
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