Adapting Temperature-Sensitive Paint Technology for Use in AEDC Hypervelocity Wind Tunnel 9-Reference-Cited by-同舟云学术

Adapting Temperature-Sensitive Paint Technology for Use in AEDC Hypervelocity Wind Tunnel 9

Published:2004-06-19 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Norris Joseph¹,Hamner Marvine²,Lafferty John³,Smith Neal⁴,Lewis Mark⁴

Affiliation:

1. Aerospace Testing Alliance

2. LeaTech LLC

3. Arnold Engineering Development Center - White Oak

4. University of Maryland

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2191

Reference9 articles.

1. Heat transfer measurement on a waverider at Mach 10 using fluorescent paint

2. Temperature- and Pressure-Sensitive Paint Measurements in Short-Duration Hypersonic Flow

3. 4Marren,D.,andLafferty,J."TheAEDCHypervelocityWindTunnel9,"AdvancedHypersonicTestFacilities,Progressin Aeronautics and Astronautics, Vol.198,AmericanInstituteofAeronauticsandAstronautics,Inc.,Reston VA,2002,pp.467-477.

Cited by 5 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. Heat Flux Measurements on the Impingement Surface of a Jet Operating at an Inclined Angle;55th AIAA Aerospace Sciences Meeting;2017-01-05

2. Investigation of Mach 10 Boundary Layer Stability of Sharp Cones at Angle-of-Attack, Part 1: Experiments;53rd AIAA Aerospace Sciences Meeting;2015-01-03

3. Heat-Flux Measurements with Temperature-Sensitive Paint in a Mach-6 Quiet Tunnel;Journal of Spacecraft and Rockets;2013-03

4. Correcting lateral heat conduction effect in image-based heat flux measurements as an inverse problem;International Journal of Heat and Mass Transfer;2011-02

5. Analytical Method for Determining Heat Flux from Temperature-Sensitive-Paint Measurements in Hypersonic Tunnels;Journal of Thermophysics and Heat Transfer;2010-01