Influence of Boundary Layer Transition on the Trajectory Optimisation of a Reusable Launch Vehicle-Reference-Cited by-同舟云学术

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Influence of Boundary Layer Transition on the Trajectory Optimisation of a Reusable Launch Vehicle

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Wuilbercq Romain¹,Pescetelli Fabrizio¹,Minisci Edmondo¹,Brown Richard E.¹

Affiliation:

1. University of Strathclyde

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2362

Reference22 articles.

1. Comments on Hypersonic Boundary-Layer Transition

2. Comparison of boundary-layer transition on a cone and flat plate at Mach 3.5

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