Isolated roughness induced boundary-layer transition - Shuttle Orbiter ground tests and flight experience-Reference-Cited by-同舟云学术

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Isolated roughness induced boundary-layer transition - Shuttle Orbiter ground tests and flight experience

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Bouslog Stanley¹,Bertin John²,Berry Scott³,Caram Jose³,Bouslog Stanley¹,Bertin John²,Berry Scott³,Caram Jose³

Affiliation:

1. Rohr, Inc., Chula Vista, CA

2. U.S. Air Force Academy, Colorado Springs, CO

3. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-274

Reference23 articles.

1. Hypersonic Boundary-Layer Transition

Cited by 22 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. Aerothermodynamics of Vehicle‐Integrated Scramjet;Scramjet Propulsion;2022-11-18

2. Numerical Method for Flow Transition Prediction;Springer Aerospace Technology;2021

3. Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool;46th AIAA Thermophysics Conference;2016-06-10

4. NASA Langley Experimental Aerothermodynamic Contributions to Slender and Winged Hypersonic Vehicles;53rd AIAA Aerospace Sciences Meeting;2015-01-03

5. Roles of Engineering Correlations in Hypersonic Entry Boundary Layer Transition Prediction;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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