Minimizing boundary layer bleed for a mixed compression inlet-Reference-Cited by-同舟云学术

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Minimizing boundary layer bleed for a mixed compression inlet

Published:1973-08-16 Issue: Volume: Page:
ISSN:
Container-title:9th Propulsion Conference
language:
Short-container-title:

Author:

WASSERBAUER J.¹,SHAW R.¹,NEUMANN H.¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1973-1270

Reference8 articles.

1. Axisymmetric Inlet With Large Transonic Mass Flow at Mach Numbers 0 6 to 2 65", TN D-6971, 1972, NASA, Moffett Field, Calif. 2. Koncsek, J.L., and Syberg, J. "Transonic and Supersonic Test of a

2. Incorporating the Method of Characteristics, 11 TND-4960, 1969, NASA, Cleveland, Ohio

Cited by 4 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. CFD Driven Aero-Propulsive Design of a Ducted Ramjet Missile;Journal of Aerospace Sciences and Technologies;2023-07-29

2. Effects of Bleed Position on the Stability of a Supersonic Inlet;Journal of Propulsion and Power;2016-09

3. Effects of Boundary-Layer Bleed Parameters on Supersonic Intake Performance;Journal of Propulsion and Power;2015-05

4. Investigation of Segmented Bleed Model in Supersonic Turbulent Boundary Layer;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

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