Further investigation of the effects of “aerodynamic ramp” design upon mixing characteristics

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Cox Stouffer, S K ^a   Gruber, M R ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; PROPULSION;

CENTERLINES; COARSER GRID; COMPUTATIONAL FLUID DYNAMICS ANALYSIS; DYNAMIC PRESSURE RATIO; FUEL INJECTORS; GRID CONVERGENCE; MIXING CHARACTERISTICS;

MIXING;

EID: 84963800732     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2238     Document Type: Conference Paper

References (9)

1. Riggins, D. and McClinton, C., “Analysis of Losses in Supersonic Mixing and Reacting Flows,” AIAA Paper 91-2266.
2. Schetz, J.A., Thomas, R.H., and Billig, F.S., “Mixing of Transverse Jets and Wall Jets in Supersonic Flow,” Separated Flows and Jets, ed. V.V. Kozlov and A.V. Dovgal. 1991, pp. 807-837.
3. Cox, S.K., Fuller, R.P., Schetz, J.A., and Walters, R. W., “Vortical Interactions Generated by an Injector Array to Enhance Mixing in Supersonic Flow,” AIAA Paper 94-0708.
4. Fuller, R.P., Wu, P.K., Nejad, A.S., and Schetz, J.A., “Comparison of Physical and Aerodynamic Ramps as Fuel Injectors in Supersonic Flow,” Journal of Propulsion and Power, Vol 14, No. 1, 1998, pp. 135-142.
5. Schetz, J.A., Cox-Stouffer, S.K., and Fuller, R.P., “Integrated CFD and Experimental Studies of Complex Injectors in Supersonic Flows,” AIAA Paper 98-2780.
6. Cox-Stouffer, S.K., and Gruber, M.R., “Effects of Spanwise Injector Spacing on Mixing Characteristics of ‘Aerodynamic Ramp’ Injectors,” AIAA Paper 98-3272.
7. Cox-Stouffer, S.K., and Gruber, M.R., “Effects of Injector Yaw On Mixing Characteristics Of ‘Aerodynamic Ramp’ Injectors,” AIAA Paper 99-0086.
8. Gruber, M.R., and Nejad, A.S., “New Supersonic Combustion Research Facility, “ Journal of Propulsion and Power, Vol. 11, No.5, 1995, pp. 1080-1083.
9. Wilcox, D.C., “Progress in Hypersonic Turbulence Modeling,” AIAA Paper 91-1785