HIFiRE-5b Boundary-Layer Transition Length and Turbulent Overshoot-Reference-Cited by-同舟云学术

HIFiRE-5b Boundary-Layer Transition Length and Turbulent Overshoot

Published:2021-03 Issue:2 Volume:58 Page:265-283
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Juliano Thomas J.¹,Jewell Joseph S.²,Kimmel Roger L.²

Affiliation:

1. University of Notre Dame, Notre Dame, Indiana 46556-5684

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7542

Funder

Defence Science and Technology Group

Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34856

Reference54 articles.

1. DolvinD. J. “Hypersonic International Flight Research and Experimentation (HIFiRE): Fundamental Sciences and Technology Development Strategy,” AIAA Paper 2008-2581, April 2008. 10.2514/6.2008-2581

2. Hypersonic International Flight Research and Experimentation Technology Development and Flight Certification Strategy

3. HIFiRE-5 Flight Vehicle Design

4. HIFiRE-5 Flight Test Preliminary Results

5. KimmelR. L.PoggieJ. “Three-Dimensional Hypersonic Boundary Layer Stability and Transition,” U.S. Air Force Research Lab. WL-TR-97-3111, Wright–Patterson Air Force Base, OH, Dec. 1997.

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