A 2-Liter, 2000 MPa Air Source for the Radiatively Driven Hypersonic Wind Tunnel (Invited)-Reference-Cited by-同舟云学术

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A 2-Liter, 2000 MPa Air Source for the Radiatively Driven Hypersonic Wind Tunnel (Invited)

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Costantino Marc¹,Lofftus Dave²,Hunter Larry²

Affiliation:

1. Lawrence Livermore National Laboratory

2. MSE

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3127

Reference7 articles.

1. Radiatively driven hypersonic wind tunnel

2. Ultra-high pressure driver and nozzle survivability in the RDHWT/MARIAH II hypersonic wind tunnel

3. Figure 7. Typical output ofa simulationusingEASY5. The dashed line isthe control velocityfor the UHP pistonand the solid line isthe model simulation. The rupture diskthat opensthe nozzle to flowfunctionsat about 0.78 sat 2000 MPa.

Cited by 2 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. Calculation of Air Chemistry in the Electron Beam Heated Hypersonic Wind Tunnel II. Current Experiments (Invited);22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2002-06-24

2. RDHWT/MARIAH II Program: Facility Performance and System Integration Issues (Invited);22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2002-06-24

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