Development of an Atmospheric-Boundary-Layer Profile at the NASA Langley Transonic Dynamics Tunnel-Reference-Cited by-同舟云学术

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Development of an Atmospheric-Boundary-Layer Profile at the NASA Langley Transonic Dynamics Tunnel

Published:2018-09-15 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA SPACE and Astronautics Forum and Exposition
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Author:

Ivanco Thomas G.¹,Keller Donald F.¹,Pinkerton Jennifer L.¹,Disotell Kevin J.²,Collins Jesse G.³,Seliquini Sky L.³

Affiliation:

1. NASA Langley Research Center

2. Youngstown State University

3. Jacobs

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5184

Reference19 articles.

1. Hanson,P. W.; and Jones, G. W. "On theUseofDynamicModelsfor StudyingLaunchVehicleBuffet and Ground-Wind Loads," NASA TM X50548, September 1963.

2. Keller, D. K.; and Ivanco, T. G. "Wind Tunnel Investigation ofGround Wind Loadsfor Ares LaunchVehicle," 28thAIAA Applied AerodynamicsConference, Chicago, IL, AIAA-2010-4371,June2010.

3. The design of spires for wind simulation

Cited by 3 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. Effect of Reynolds Number and Aeroelastic Scaling Upon Launch-Vehicle Ground-Wind Loads;Journal of Spacecraft and Rockets;2024-07-09

2. Simulation of Atmospheric Boundary Layer for Air Inlet Testing in Crossflow;AIAA Journal;2021-07

3. Wind Tunnel to Full Scale Mapping of Winds and Loads for Launch-Vehicle Ground Wind Loads;AIAA Scitech 2021 Forum;2021-01-04

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