Optical refraction from high mach number turbulent boundary layer structures

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Erbland, P J ^a   Etz, M R ^b   Lempert, W R ^b   Smits, A J ^b   Miles, R B ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Princeton University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; HELIUM; HIGH ENERGY LASERS; MACH NUMBER; REFRACTION; TURBULENCE; WIND TUNNELS;

EXPERIMENTAL AND NUMERICAL STUDIES; FIRST-ORDER SENSITIVITY; HYPERSONIC WIND TUNNELS; OPTICAL REFRACTION; PRELIMINARY ANALYSIS; TURBULENT BOUNDARY LAYER STRUCTURE; TURBULENT BOUNDARY LAYERS; TURBULENT STRUCTURES;

ATMOSPHERIC THERMODYNAMICS;

EID: 84982318228     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-399     Document Type: Conference Paper

References (8)

1. R. B. Miles, G. L. Brown, W. R. Lempert, R. A. Yetter, G. J. Williams, S. M. Bogdonoff, "Radiatively Driven Hypersonic Wind Tunnel," AIAA Journal, 33, No. 8, p. 1463, August 1995.
2. G. Havener, "Computational Flow Imaging: Fundamentals and History," AIAA-94-2615, 18th AIAA Aerospace Ground Testing Conference, June, 1994.
3. G. L. Brown, A. P. Ratta, R. W. Anderson, L. Martinelli, W. R. Lempert, and R. B. Miles, "Fluid Mechanics in a Radiatively Driven Hypersonic Wind-Tunnel-Prediction and Preliminary Experiment," AIAA-96-2199, 19th AIAA Advanced Measurement and Ground Testing Technology Conference, June, 1996.
4. Etz, M. R. "The Effects of Transverse Sonic Gas Injection on a Hypersonic Boundary Layer," MSE Thesis 3009T, Princeton University, 1998.
5. Erbland, P. J., et al., "Development of Planar Diagnostics for Imaging Mach 8 Flowfields Using Carbon Dioxide and Sodium Seeding," AIAA-97-0154, 35th Aerospace Sciences Meeting, January, 1997.
6. Yalin, A. P., Lempert, W. R., Eíz, M. R., Erbland, P. J., Smits, A. J., and Miles, R. B., "Planar Imaging in a Mach 8 Flow Using Sodium Laser-Induced Fluorescence," AIAA-96-2270, 19th AIAA Advanced Measurement and Ground Testing Technology Conference, June, 1996.
7. Smith, M. W., and Smits, A. J., "Visualization of the Structure of Supersonic Turbulent Boundary Layers," Experiments in Fluids, No. 18, 1995, pp. 288-302.
8. R. More, "Private Communication," Lawrence Livermore National Laboratory, Livermore, CA, 1995.