Boundary layer development downstream of a bleed mass flow removal region-Reference-Cited by-同舟云学术

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Boundary layer development downstream of a bleed mass flow removal region

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Willis B.¹,Davis D.¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3278

Cited by 12 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. Experimental and numerical investigation of porous bleed control for supersonic/subsonic flows, and shock-wave/boundary-layer interactions;Aerospace Science and Technology;2024-04

2. Effects of Boundary-Layer Bleed Slots on a Sidewall Compression Inlet;AIAA SCITECH 2023 Forum;2023-01-19

3. Parameter Influence on the Porous Bleed Performance with & without Shock-Boundary Layer Interaction;AIAA AVIATION 2022 Forum;2022-06-20

4. Computational Modelling and Analysis of Porous Bleed Holes at Supersonic Speeds;AIAA Propulsion and Energy 2020 Forum;2020-08-17

5. Effect of Inlet Boundary Layer Suction on Flow Distortion in Subsonic Diffusing S-Duct;International Journal of Aeronautical and Space Sciences;2019-05-24

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