The Prop-Fan - A new look in propulsors-Reference-Cited by-同舟云学术

The Prop-Fan - A new look in propulsors

Published:1975-08-16 Issue: Volume: Page:
ISSN:
Container-title:11th Propulsion Conference
language:
Short-container-title:

Author:

ROHRBACH C.¹,METZGER F.¹

Affiliation:

1. United Technologies Corp., Hamilton Standard Div., Windsor Locks, Conn.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1975-1208

Reference10 articles.

1. Grose, R. M. "Wind 7hnnel Siudics of thc Effects of Blade Thickncss Ratio. Camkr and Pitch Pistrihution on the Pcrformancc of Model High-Speed Propellers. *$ United Aircraft Corporation Research Dept. Rcport R-25GG5-2, June 1955.

2. Simmonrls, A. W. "Wind Tunnel Tcst of Variable Cambcr and Conventional Model Propellers, United Aircraft Corporation Research Pcpt. Report B33034-1. Deccmber 1963.

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. Numerical investigation for the performance enhancement of propeller propulsion systems;THE 8TH ANNUAL INTERNATIONAL SEMINAR ON TRENDS IN SCIENCE AND SCIENCE EDUCATION (AISTSSE) 2021;2022

2. GasProp: Reducing Blade Compressibility Effects Through Waste-Heat Recovery in Aircraft Engines;AIAA Journal;2020-02

3. Open-rotor noise prediction with a RANS-informed analytical method;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04

4. Laser-velocimeter flow-field measurements of an advanced turboprop;17th Joint Propulsion Conference;1981-07-27

5. Comparisons of alternate energy efficient engines for future subsonic transports as affected by engine technology improvements;12th Propulsion Conference;1976-07-26