Comparison of Ares I-X Wind-Tunnel Derived Buffet Environment with Flight Data-Reference-Cited by-同舟云学术

Comparison of Ares I-X Wind-Tunnel Derived Buffet Environment with Flight Data

Published:2011-06-27 Issue: Volume: Page:
ISSN:
Container-title:29th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Piatak David¹,Sekula Martin¹,Rausch Russ¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3013

Reference15 articles.

1. Jones, George W., Foughner, Jerome T., Jr. "Investigation of Buffet Pressures on Models of Large Manned LaunchVehicle Configurations". NASATN-D-1663, May1963.

2. Progress on the launch-vehicle buffeting problem

3. Cole, Henry A., Jr.; Erickson, A. L.; and Rainey, A. G. "Buffeting During Atmospheric Ascent". NASA SP8001,1963, Revised November 1970.

4. Piatak, D. J., etal, "Test SummaryDocument for the 3.5 Percent AresI-X Rigid Buffet Model". ARES-AE-TA0002,Version1.0,July11, 2008.

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. Developmental Flight Instrumentation: Review of Space Shuttle, Ares I-X, and Artemis I;AIAA SCITECH 2024 Forum;2024-01-04

2. Scaling procedures of cabin noise generated by turbulent boundary layer excitation;Chinese Journal of Aeronautics;2018-03

3. Effect of a Protuberance on Transonic Flowfield around a Rocket Fairing;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2013

4. Hybrid LES/RANS Simulations of Transonic Flowfield Around a Rocket Fairing;30th AIAA Applied Aerodynamics Conference;2012-06-25

5. Asymmetric Uncertainty Expression for High Gradient Aerodynamics;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09