Free-Flight Aerodynamic Testing of the Skylon Space Plane-Reference-Cited by-同舟云学术

Free-Flight Aerodynamic Testing of the Skylon Space Plane

Published:2021-09 Issue:5 Volume:58 Page:1487-1497
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Hyslop Andrew,Doherty Luke J.,McGilvray Matthew,Neely Andrew,McQuellin Liam P.,Barth James,Mullen Gerrie

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34937

Reference22 articles.

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

2. Hypersonic Boundary-Layer Transition

3. Hypersonic aerodynamic characteristics for Langley Test Technique Demonstrator

4. LiuS. K. “Numerical Simulation of Hypersonic Aerodynamics and the Computational Needs for the Design of an Aerospace Plane,” RAND Corp., Tech. Rept. Santa Monica, CA, 1992.

5. The SKYLON Project

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