Mach 10 Rayleigh Scattering Gas-Cap Density, Pressure, and Shock-Jump Measurements-Reference-Cited by-同舟云学术

Mach 10 Rayleigh Scattering Gas-Cap Density, Pressure, and Shock-Jump Measurements

Published:2015-03 Issue:3 Volume:53 Page:756-762
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Balla R. Jeffrey¹

Affiliation:

1. Advanced Sensing and Optical Measurement Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053698

Reference13 articles.

1. Laser Rayleigh scattering

2. Rayleigh Scattering Density Measurements, Cluster Theory, and Nucleation Calculations at Mach 10

3. Supersaturation Total Temperature, Pitot Pressure, and Rayleigh Scattering Measurements at Mach 10

4. Rayleigh scattering measurements in supersonic facilities

5. HollisB. R. “Real-Gas Flow Properties for NASA Langley Research Center Aerothermodynamic Facilities Complex Wind Tunnels,” NASA CR-4755, Sept. 1996.

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