Reflection of large amplitude acoustic pulses from an axial flow compressor-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Reflection of large amplitude acoustic pulses from an axial flow compressor

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Freund Donald¹,Sajben Miklos¹,Freund Donald¹,Sajben Miklos¹

Affiliation:

1. Cincinnati, Univ., OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2879

Reference17 articles.

1. Domack, C.S."A Preliminary Investigation of Inlet Unstart Effects on a High-Speed Civil Transport Concept," AIAA paper 91-3327.

2. Chung, J. and Cole, G.L. "Comparison of Compressor Face Boundary Conditions for Unsteady CFD Simulations of Supersonic Inlets," AIAA paper 95-2627.

3. Mayer, W.D.and Paynter, G.C. "Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances,"AIAA paper 94-0580.

4. Decher, R., Mayer, D.W.and Paynter, G.C."On Supersonic Inlet-Engine Stability," AIAA paper 94-3371.

5. Boundary conditions for unsteady supersonic inlet analyses

Cited by 3 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. Implementation of a Compressor Face Boundary Condition Based on Small Disturbances;Journal of Turbomachinery;2000-02-01

2. Analysis of inlet-compressor acoustic interactions using coupled CFD codes;37th Aerospace Sciences Meeting and Exhibit;1999-01-11

3. Unsteady Inlet/Compressor Interaction Experiment to Support the Modeling of Compressor-Face Boundary Conditions;Unsteady Aerodynamics and Aeroelasticity of Turbomachines;1998

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370

www.globalauthorid.com

TOP