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Computational Study of Submerged Air Inlet Performance Improvement Using Vortex Generators

  • Published:2007-09 Issue:5 Volume:44 Page:1574-1587
  • ISSN:0021-8669
  • Container-title:Journal of Aircraft
  • language:en
  • Short-container-title:Journal of Aircraft

Author:

Pérez César Celis,Ferreira Sandro Barros,da Silva Luís Fernando Figueira,de Jesus Antônio Batista,Oliveira Guilherme Lara

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 16 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. Investigating the Effects of Vortex Generator Geometry on NACA Inlet Performance;CFD Letters;2024-08-31

2. The study of cascading effect in the integration of intake with gas turbine engine bay in subsonic cruise vehicle;International Journal of Turbo & Jet-Engines;2024-08-19

3. Design Optimization of a Novel Flush Boundary Layer Diverter;Journal of Turbomachinery;2024-07-15

4. Design and analysis of air intake of subsonic cruise vehicle with experimental validation;International Journal of Turbo & Jet-Engines;2024-04-04

5. Aerodynamic efficiency analysis of the ridge integrated submerged inlet;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-01-16
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