Bleed system design technology for supersonic inlets-Reference-Cited by-同舟云学术

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Bleed system design technology for supersonic inlets

Published:1972-08-16 Issue: Volume: Page:
ISSN:
Container-title:8th Joint Propulsion Specialist Conference
language:
Short-container-title:

Author:

SYBERG J.¹,KONCSEK J.¹

Affiliation:

1. Boeing Co., Seattle, Wash.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1972-1138

Reference7 articles.

1. of the SST Prototype Air Intake, report FAA-SS-72-50.

2. A procedure for combined viscous-inviscid analysis of supersonic inlet flow fields

Cited by 9 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. Aerothermal characteristics of bleed slot in hypersonic flows;Science China Physics, Mechanics & Astronomy;2015-09-05

2. Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward High- light and Bleed Slot in an Inverted “X”-type Layout;Chinese Journal of Aeronautics;2007-08

3. Supersonic-inlet boundary-layer bleed flow;AIAA Journal;1996-04

4. Shock-wave/boundary-layer interactions with bleed. II - Effect of slot location;Journal of Propulsion and Power;1995-11

5. Shock-wave/boundary-layer interactions with bleed. I - Effect of slot angle;Journal of Propulsion and Power;1995-11

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