Study of injection of helium into supersonic air flow using rayleigh scattering

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Seasholtz, R G ^a   Buggele, A E ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; CCD CAMERAS; DATA VISUALIZATION; NEODYMIUM LASERS; PULSED LASERS; RAYLEIGH SCATTERING;

ABSORPTION CELLS; FILTERED RAYLEIGH SCATTERING; LASER LIGHTS; MOLE FRACTION; ND:YAG PULSED LASER; STATIC PRESSURE DATA; TRANSVERSE INJECTION; VISUALIZATION IMAGES;

HELIUM;

EID: 84983196538     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (30)

1. Borowski, S.K. and Cassenti, B.N., "Nuclear Thermal Propulsion", Aerospace America, December 1995, p. 49.
2. Rogers,R.C., "A Study of the mixing of hydrogen injected normal to a supersonic airstream", NASA TN D-6114, 1971.
3. Fuller, E.J., Mays, R.B., Thomas, R.H., and Schetz, J.A., "Mixing Studies of Helium in Air at High Supersonic Speeds", AIAA Journal, Vol. 30, № 9,1992, pp. 2234-2243.
4. Hermanson, J.C., and Winter, M., "Mie Scattering Imaging of a Transverse, Sonic Jet in Supersonic Row", AIAA Journal, Vol. 31, № 1,1993, pp. 129-132.
5. Gruber, M.R., Nejad, A.S., Chen, T.H., and Button, J.C., "Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream", Journal of Propulsion and Power, Vol. 11, № 2,1995, pp. 315-323.
6. Island, T.C., Patrie, B.J., Mungal, M.G., and Hanson, R.K., "Instantaneous Three-Dimensional Flow Visualization of a Supersonic Mixing Layer", Experiments in Fluids, Vol. 20, 1996, pp. 249-256.
7. Escoda, M.C., and Long, M.B., "Rayleigh Scattering Measurements of the Gas Concentration Field in Turbulent Jets", AIM Journal, Vol. 21, № 1,1983, pp. 81-84.
8. McDaniel, J.C., and Graves, J., Jr., "Laser-Induced-Fluorescence Visualization of Transverse Injection in a Nonreacting Supersonic Combustor", Journal of Propulsion and Power, Vol. 4, № 6, 1988, pp. 591-597.
9. Hollo, S.D., McDaniel, J.C., and Hartfield, R.J. Jr., "Characterization of Supersonic Mixing in a Nonreacting Mach 2 Combustor", AIAA 30th Aerospace Sciences Meeting, Reno, NV, AIAA paper 92-0093, 1992.
10. Wang, K.C., Smith, O.I., and Karagozian, A.R., "In-Flight Imaging of Transverse Gas Jets Injected into Compressible Crossflows",‘AIM Journal, Vol. 33, № 12, 1995, pp. 2259-2263.
11. Lee, M.P., McMillin, B.K., Palmer, J.L., and Hanson, R.K., "Planar Fluorescence Imaging of a Transverse Jet in a Supersonic Crossflow", Journal of Propulsion and Power, Vol. 8, № 4, 1992, pp. 729-735.
12. Zukoski, E.E., and Spaid, F.W., "Secondary Injection of Gases into a Supersonic Flow", AIM Journal, Vol. 2, № 10, 1964, pp. 1689-1696.
13. Papamoschou, D, and Hubbard, D.G., "Visual Observations of Supersonic Transverse Jets", Experiments in Fluids, Vol. 14, 1993, pp. 468-476.
14. McCann, G.J., and Bowersox, R.D.W., "Experimental Investigation of Supersonic Gaseous Injection into a Supersonic Freestream", AIM Journal, Vol. 34, № 2, 1996, pp. 317-322.
15. Schetz, J.A., and Billig, F.S., "Penetration of Gaseous Jets Injected into a Supersonic Stream", Journal of Spacecraft, Vol. 3, № 11, 1966, pp. 1658-1665.
16. Fuller, E.J., Mays, R.B., Thomas, R.H., and Schetz, J.A., "Mixing Studies of Helium at High Supersonic Speeds", AIM Journal, Vol. 30. № 9, 1992, pp. 2234-2243.
17. deGroot, W.A., Latham, R., Jagoda, J.I., Strahle, W.C., "Rayleigh Measurements of Species Concentration in a Complex Turbulent Flow", AIAA Journal, Vol. 25, № 8, 1987, pp. 1142-1144.
18. Everson, R., Manin, D., Sirovich, L., and Winter, M., "Quantification of Mixing Rate from Experimental Observations", AIAA 33th Aerospace Sciences Meeting, Reno, NV, AIAA paper 95-0169, 1995.
19. Graham, S.C., Grant, A.J., and Jones, J.M., "Transient Molecular Concentration Measurements in Turbulent Flows Using Rayleigh Light Scattering", AIM Journal, Vol. 12, № 8, 1974, pp. 1140-1142.
20. Goix, P.J., Leonard, K.R., Talbot, L., and Chen, J.Y., "Direct Measurement of Mixture Fraction in Reacting Flow using Rayleigh Scattering", Experiments in Fluids, Vol. 15, 1993, pp. 247-254.
21. Stepowski, D. and Cabot, G., "Single-Shot Temperature and Mixture Fraction Profiles by Rayleigh Scattering in the Development Zone of a Turbulent Diffusion Flame", Combustion and Flame, Vol. 88, 1992, pp. 296-308.
22. Long, M.B., Levin, P.S., and Fourguette, D.C., "Simultaneous Two-Dimensional Mapping of Species Concentration and Temperature in Turbulent Flames", Optics Letters, Vol. 10, № 6, 1985, pp. 267-269.
23. Dyer, T.M., "Rayleigh Scattering Measurements of Time-Resolved Concentration in a Turbulent Propane Jet", AIAA Journal, Vol. 17, № 8,1979, pp. 912-914.
24. Miles, R., and Lempert, W., "Flow Diagnostics in Unseeded Air", AIAA 28th Aerospace Sciences Meeting, Reno, NV, AIAA paper 90-0624, 1990.
25. Forkey, J.N., Finkelstein, N.D., Lempert, W.R. & Miles, R.B., "Demonstration and Characterization of Filtered Rayleigh Scattering for Planar Velocity Measurements", AIM Journal, Vol. 34, № 3, 1996, pp. 442-448.
26. Forkey, J.N., "Development and Demonstration of Filtered Rayleigh Scattering - A Laser Based Row Diagnostic for Planar Measurement of Velocity, Temperature and Pressure", Ph.D. dissertation #2067-T, Princeton University, 1996.
27. Hoffman, D., Munch, K.-U., and Leipertz, A., ‘Two-Dimensional Temperature Determination in Sooting Flames by Filtered Rayleigh Scattering", Optics Letters, Vol. 21, № 7, 1996, pp. 525-527.
28. Kingslake, R., Optical System Design, Academic Press, New York, 1983, pp. 265-272.
29. Seasholtz, R.G., Buggele, A.E., & Reeder, M.F., "Instantaneous Flow Measurements in a Supersonic Wind Tunnel Using Spectrally Resolved Rayleigh Scattering", SPIE International Symposium on Optical Science, Engineering, and Instrumentation, San Diego, CA, July 9-14, 1995.
30. Decker, A.J., and Buggele, A.E., "Automation of Some Operations of a Wind Tunnel Using Artificial Neural Networks", AIM Journal, Vol. 34, № 2, 1996, pp. 421-423.