Reacting hypersonic boundary layer stability with blowing and suction

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Johnson, Heath B ^a   Gronvall, Joel E ^a   Candler, Graham V ^a  

^a University of Minnesota   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CARBON DIOXIDE; COMPUTATIONAL FLUID DYNAMICS; ENTHALPY; HYPERSONIC FLOW; LINEAR STABILITY ANALYSIS;

AMPLIFICATION RATE; CFD SIMULATIONS; COMPUTATIONAL RESULTS; LOW ENTHALPIES; STABILITY ANALYSIS; STABILIZING EFFECTS; SUCTION EFFECTS; TRANSITION LOCATIONS;

HYPERSONIC BOUNDARY LAYERS;

EID: 78549287538     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-938     Document Type: Conference Paper

References (14)

1. S. Schneider. Hypersonic Boundary-Layer Transition with Ablation and Blowing. Technical Report 2008-3730, AIAA, June 2008.
2. C.C. Pappas and A.F. Okuno. Measurements of Skin Friction of the Compressible Turbulent Boundary Layer on a Cone With Foreign Gas Injection. J. of the Aero/Space Sciences, 27(5):321-333, May 1960.
3. H. B. Johnson and G. V. Candler. Hypersonic Boundary Layer Stability Analysis Using PSE-Chem. Paper 2005-5023, AIAA, June 2005.
4. M. J. Wright, G. V. Candler, and D. Bose. A Data-Parallel Line-Relaxation Method for the Navier-Stokes Equations. Paper 97-2046CP, AIAA, June 1997.
5. H. B. Johnson and G. V. Candler. Analysis of Laminar-Turbulent Transition in Hypersonic Flight using PSE-Chem. Paper 2006-3057, AIAA, June 2006.
6. C. R. Alba, H. B. Johnson, and G. V. Candler. Oblique Wave Disturbance Analysis of Supersonic Flow Past Axisymmetric and 2D Bodies at Angles of Attack. Paper 2008-4396, AIAA, June 2008.
7. R. Gosse and G. V. Candler. Evaluation of Carbon-Carbon Ablation Models Using a Fully Coupled CFD Solver. Paper 2008-3908, AIAA, June 2008.
8. Mujeeb R. Malik. Prediction and Control of Transition in Supersonic and Hypersonic Boundary Layers. AIAA Journal, 27(11):1487-1493, November 1989.
9. C.C. Pappas and A.F. Okuno. Heat Transfer For Binary Gas Laminar Boundary Layers With High Rates Of Injection. Technical Note TN-D-2473, NASA, September 1964.
10. M.R. Malik, R.E. Spall, and C.-L. Chang. Effect of Nose Bluntness on Boundary Layer Stability and Transition. Paper 90-0112, AIAA, January 1990.
11. J. Stilla. Engineering Transition Prediction for a Hypersonic Axisymmetric Boundary Layer. Journal of Aircraft, 31(6):1358-1364, November 1994.
12. H. B. Johnson, T. G. Seipp, and G. V. Candler. Numerical Study of Hypersonic Reacting Boundary Layer Transition on Cones. Physics of Fluids, 10(10):2676-2685, October 1998.
13. H. Johnson, C. Alba, G. Candler, M. MacLean, T. Wadhams, and M. Holden. Boundary Layer Stability Analysis to Support the HIFiRE Transition Experiment. Paper 2007-311, AIAA, January 2007. Also to appear in Journal of Spacecraft and Rockets.
14. H. B. Johnson, T. G. Seipp, and G. V. Candler. Numerical Study of Hypersonic Reacting Boundary Layer Transition on Cones. Paper 1997-2567, AIAA, June 1997.