Predicted vs. scale model and flight test UDF engine noise-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Predicted vs. scale model and flight test UDF engine noise

Published:1990-08-17 Issue: Volume: Page:
ISSN:
Container-title:13th Aeroacoustics Conference
language:
Short-container-title:

Author:

WHITFIELD C.¹,GLIEBE P.¹

Affiliation:

1. GE Aircraft Engines, Cincinnati, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-3936

Reference18 articles.

1. H E. Nichols. UDF Engine/MD-80 Program. AIAA 88-2805, July 1988.

2. G.E. Hoff, Experimental Performance and Acoustic Investigation of Modern Counterrotating Blade Concepts. NASA Contractor Report CR-185158, GE Aircraft Engines, January 1990.

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. Influence of Torque Ratio on Counter-Rotating Open-Rotor Interaction Noise;AIAA Journal;2015-09

2. Influence of Torque Ratio on Counter Rotating Open Rotor Interaction Noise;20th AIAA/CEAS Aeroacoustics Conference;2014-06-13

3. Prediction of Tonal Aerodynamic Noise from Open Rotors;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04

4. Rotor-rotor interaction for counter-rotating fans. I - Three-dimensional flowfield measurements;AIAA Journal;1994-11

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