Boundary layer suction for high-speed air intakes: A review-Reference-Cited by-同舟云学术

Boundary layer suction for high-speed air intakes: A review

Published:2018-08-13 Issue:9 Volume:233 Page:3459-3481
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Sepahi-Younsi Javad¹^ORCID,Forouzi Feshalami Behzad¹,Maadi Seyed Reza¹,Soltani Mohammad Reza²

Affiliation:

1. Mechanical Engineering Department, Faculty of Engineering, Ferdowsi University of Mashhad, Mashad, Iran

2. Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran

Abstract

The paper summarizes recent developments in boundary layer suction for high-speed air intakes. Bleed has been efficiently used in supersonic and hypersonic intakes for three primary reasons: to improve the performance of the intake, to reduce the starting Mach number of the intake, and to postpone the onset of buzz oscillations. A bleed system has many characteristics such as the bleed entrance and exit areas, bleed entrance slant angle and position, and bleed type (slot or porous and ram-scoop or flush). Each of these parameters has significant impacts on the intake performance and stability that have been reviewed in this study. In addition, the effectiveness of other flow control methods has been compared with the bleed method.

Funder

Ferdowsi University of Mashhad

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/0954410018793262

Reference59 articles.

1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?

Cited by 36 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. 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

2. Numerical Investigations of Bump Effects on the Performance of Double-Ended Airfoils and ABC Rotors;International Journal of Aeronautical and Space Sciences;2023-12-02

3. Prediction model based on artificial neural network and bivariate spectral quasi-linearization method for compressible turbulent boundary-layer flow over a smooth flat surface;Physics of Fluids;2023-12-01

4. Starting of a scramjet air intake;Aerospace Science and Technology;2023-10

5. Boundary layer suction timing and location effects on unstarting flows in a model scramjet;Aerospace Science and Technology;2023-09