Expanded Measurement Capabilities at the AEDC Hypervelocity Wind Tunnel No. 9-Reference-Cited by-同舟云学术

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Expanded Measurement Capabilities at the AEDC Hypervelocity Wind Tunnel No. 9

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Lewis Daniel¹,Coblish Joseph²

Affiliation:

1. Aerospace Testing Alliance

2. Arnold Engineering Development Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4791

Reference10 articles.

1. 3Kurits,I.,Lewis,M.J.,andHamner,M.P."GlobalHeat-TransferMeasurementsontheNASACrewExplorationVehicleat AEDCTunnel9," AIAA2008-3947, June2008.

2. 4Kurits,I.,Norris,J.D."HypersonicGlobalHeat-TransferMeasurementsDuringContinuousPitchSweepsatAEDCTunnel9," AIAA2010-4802, June2010.

Cited by 2 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. Boundary-Layer Transition Induced by an Isolated Roughness Element in Mach 6 Quiet Flow;AIAA SCITECH 2024 Forum;2024-01-04

2. The Hypervelocity Wind Tunnel No. 9; Continued Excellence Through Improvement and Modernization;53rd AIAA Aerospace Sciences Meeting;2015-01-03

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