Measurements to Assess the Degree of Thermal Nonequilibrium at AEDC Hypervelocity Wind Tunnel No. 9

Author:

Smith Michael1,Coblish Joseph1

Affiliation:

1. Arnold Engineering Development Center

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. 1Candler,G.V.,etal."CFDValidationforHypersonicFlight:HypersonicDouble-ConeFlowSimulations,"AIAA Paper 2002-0581, January 2002

2. 3Lafferty, J. F., and Marren, D.E. "Hypervelocity Wind Tunnel No. 9 Mach 7 Thermal Structural Facility Verification and Calibration." Technical Report NSWCDD/TR-95/231, Naval Surface Warfare Center, Silver Spring, MD 20903-5640,June1996.

3. 4Swinford, N. F. "Hypervelocity Wind Tunnel 9 Mach 8 Calibration," Technical Report NSWCDD/TR-93/40, NavalSurface Warfare Center,SilverSpring,MD20903-5640, June 1994.

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1. The Hypervelocity Wind Tunnel No. 9; Continued Excellence Through Improvement and Modernization;53rd AIAA Aerospace Sciences Meeting;2015-01-03

2. Supersaturation Total Temperature, Pitot Pressure, and Rayleigh Scattering Measurements at Mach 10;AIAA Journal;2014-07

3. Effect of Water Vapor on the AEDC Tunnel 9 Mach 14 Nozzle Flow;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

4. Raman Density and Gas-Sampling Measurements During Tunnel 9 Mach 8 Calibration;25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2006-06-05

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