Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations-Reference-Cited by-同舟云学术

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Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations

Published:1988-07-11 Issue: Volume: Page:
ISSN:
Container-title:24th Joint Propulsion Conference
language:
Short-container-title:

Author:

HUGHES CHRISTOPHER¹,GAZZANIGA JOHN²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. NASA, Lewis Research Center; Sverdrup Technology,Inc., Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-3149

Reference23 articles.

1. A Model Propulsion Simulator for Evaluating Counterrotating Blade Characteristics

2. Unducted Fan Aerodynamic Design

Cited by 5 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. Historical development of the coaxial contra-rotating propeller;The Aeronautical Journal;2022-11-25

2. Influence of Variable Geometry Compressor on Transient Performance of Counter-Rotating Open Rotor Engines;Journal of Engineering for Gas Turbines and Power;2018-08-13

3. A Propeller Model for Steady-State and Transient Performance Prediction of Turboprop and Counter-Rotating Open Rotor Engines;Journal of Engineering for Gas Turbines and Power;2018-04-20

4. Nearfield Unsteady Pressures at Cruise Mach Numbers for a Model Scale Counter-rotation Open Rotor;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04

5. Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack;25th Joint Propulsion Conference;1989-07-12

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