Advanced nozzle and engine components test facility-Reference-Cited by-同舟云学术

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Advanced nozzle and engine components test facility

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:17th Aerospace Ground Testing Conference
language:
Short-container-title:

Author:

BELTRAN LUIS¹,DEL ROSO RICHARD¹,DE RUBEN¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3993

Cited by 6 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. Aerodynamic performance of augmented supersonic nozzles;Experiments in Fluids;2020-01-21

2. A new thrust stand for testing multi-stream and heat simulated supersonic nozzles;54th AIAA Aerospace Sciences Meeting;2016-01-02

3. Drag Measurements of Porous Plate Acoustic Liners;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

4. Review of research into the concept of the microblowing technique for turbulent skin friction reduction;Progress in Aerospace Sciences;2004-11

5. Advanced Nozzle Test Facility at NASA Glenn Research Center's Engine Research Building (Invited);22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2002-06-24

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