Characterization of a Ludwieg Tube with Free Piston Compression Heating in Mach 6 Configuration-Reference-Cited by-同舟云学术

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Characterization of a Ludwieg Tube with Free Piston Compression Heating in Mach 6 Configuration

Published:2018-09-15 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
language:
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Author:

Birch Byrenn¹,Buttsworth David¹,Choudhury Rishabh¹,Stern Nathan¹

Affiliation:

1. University of Southern Queensland

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5266

Reference30 articles.

1. Experimental determination of the free-stream disturbance field in a short-duration supersonic wind tunnel

2. Development of Hypersonic Quiet Tunnels

3. Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind Tunnels

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1. Commissioning Ludwieg Mode with Isentropic Compression Heating for the Oxford High Density Tunnel;AIAA SCITECH 2024 Forum;2024-01-04

2. Roll and Pitch Control of a Hypersonic Wind Tunnel Model with Actuated Canards;AIAA SCITECH 2024 Forum;2024-01-04

3. Optical aerodynamic measurements of hypersonic free-flight using Bayesian state estimation;AIAA AVIATION 2023 Forum;2023-06-08

4. Oscillating shock wave boundary layer interactions on a cantilever plate;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27

5. Wind-Tunnel based Free-Flight Testing of a Viscous Optimised Hypersonic Waverider;AIAA SCITECH 2023 Forum;2023-01-19

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