Role of bypass transition in conventional hypersonic facilities

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  McDaniel, R D ^a   Hassan, H A ^a  

^a North Carolina State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; HEAT TRANSFER; REYNOLDS NUMBER; WIND TUNNELS;

BYPASS TRANSITION; HEAT TRANSFER MEASUREMENTS; HYPERSONIC WIND TUNNELS; ZERO ANGLE;

ANGLE OF ATTACK;

EID: 85088344970     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-209     Document Type: Conference Paper

References (17)

1. Warren, E. S. and Hassan, H. A., "An Alternative to the / Method for Determining Onset of Transition, " AIAA Paper 97-0825, January 1997.
2. Warren, E. S. and Hassan, H. A., "A Transition Model for Swept Wing Flows, " AIAA Paper 97-2245, June 1997.
3. Warren, E. S. and Hassan, H. A., "Transition Closure Model for Predicting Transition Onset, " Journal of Aircraft, Vol. 35, No. 5, September-October 1998, pp. 769-775.
4. McDaniel, R. D. and Hassan, H. A., "Study of Bypass Transition Using the k-ζ Framework, " AIAA Paper 2000-2310, June 2000.
5. Savill, A. M., "One Point Closures Applied to Transition, " in Turbulence and Transition Modeling, edited by Hallback, M., Henningson, D. S., Johansson, A. V., and Alfredson, P. H., Kluwer Academic Publishers, Boston, 1996, pp. 233-268.
6. Stetson, K. F. and Kimmel, R. L., "On Hypersonic Boundary-Layer Stability, " AIAA Paper 92-0737, January 1992.
7. Pate, S. R. "Effects of Wind Tunnel Disturbances on Boundary-Layer Transition with Emphasis on radiated Noise: A review, " AIAA Paper 80-0431, March 1980.
8. Lachowicz, J. T., Chokani, N., and Wilkins, S. P., "Boundary-Layer Stability Measurements in Hypersonic Quiet Tunnel, " AIAA Journal, Vol. 34, No. 12, December 1996, pp. 2496-2500.
9. McDaniel, R. D., Nance, R. P., and Hassan, H. A., "Transition Onset Prediction for High Speed Flow, " Journal of Spacecraft and Rockets, Vol. 37, No. 3, May-June 2000, pp. 304-309.
10. Kimmel, R. L., "The Effect of Pressure Gradients on Transition Zone Length in Hypersonic Boundary Layers, " Journal of Fluids Engineering, Vol. 119, March 1997, pp. 36-41.
11. Donaldson, J. and Coulter, S., "A Review of Free-Stream Flow Fluctuation and Steady-State Flow Quality Measurements in the AEDC/VKF Supersonic Tunnel A and Hypersonic Tunnel B, " AIAA Paper 95-6137, April 1995.
12. Czerwiec, R. M., Edwards, J. R., Rumsey, C. L., Bertelrud, A., and Hassan, H. A., "Study of High-Lift Configurations using k-ζ Transition/Turbulence Model" AIAA Paper 99-3186, June 1999.
13. Mack, L. M., "Boundary Layer Linear Stability Theory, " in AGARD-R-709, June 1986, pp. 3.1-3.81.
14. Blanchard, A. E., Lachowicz, J. T., and Wilkinson, S. P., "NASA Langley Mach 6 Quiet Wind-Tunnel Performance, " AIAA Journal, Vol. 35, No. 1, January 1997, pp. 23-28.
15. Dhawan, S. and Narasimha, R., "Some Properties of Boundary Layer Flow During Transition from Laminar to Turbulent Motion, " Journal of Fluid Mechanics, Vol. 3, No. 4, 1958, pp. 414-436.
16. Mayle, R. E., "The Role of Laminar-Turbulent Transition in Gas Turbine Engines, " Journal of Turbomachinery, Vol. 113, July 1991, pp. 509-537.
17. Olynick, D. P. and Hassan, H. A., "A New Two-Temperature Dissociation Model for Reacting Flows, " Journal of Thermophysics and Heat Transfer, Vol. 7, No. 4, October-December 1993, pp. 687-696.