Evaluation of the A320 hybrid laminar fin experiment

European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2000

Volumn , Issue , 2000, Pages

  Schrauf, Géza H ^a  

^a AIRBUS OPERATIONS GMBH   (Germany)

Author keywords

Boundary layer suction; EN method; Hybrid laminar flow; Laminar turbulent transition; Linear stability theory; Transition prediction

Indexed keywords

BOUNDARY LAYER SUCTION; EN-METHOD; LAMINAR-TURBULENT TRANSITION; LINEAR STABILITY THEORY; TRANSITION PREDICTION;

AMPLIFICATION; BOUNDARY LAYERS; COMPUTATIONAL METHODS; EXPERIMENTS; FINS (HEAT EXCHANGE); LAMINAR FLOW; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS;

VERTICAL STABILIZERS;

EID: 84878492686     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. R. Henke, A320 HLF FIN Flight Tests Completed. Air&Space Europe Vol. 1 No 2, 78-79, 1999.
2. Arnal, D., Boundary Layer Transition: Predictions based on Linear Theory. In: Special Course on Progress in Transition Modeling AGARD Report N0. 793, 1994, pp. 21 - 263.
3. Schrauf, G., Perraud, J., Vitiello, D., Lam, F., Stock, H.W., Abbas, A., Transition Prediction with Linear Stability Theory. Lessons Learned from the ELFIN F100 Flight Demonstrator. 2nd European Forum on Laminar Flow Technology, 10-12. 6. 1996, Bordeaux.
4. Arnal, D., EUROTRANS Final Report. February 2000.
5. Schrauf, G., Perraud, J., Vitiello, D., Lam, F., Comparison of boundary layer transition prediction using flight test data, AIAA Journal of Aircraft Vol. 53, No. 6. November- December 1998, pp. 891-897.
6. G. Schrauf Evaluation of the ELFIN II HLF Experiments with Linear Stability Theory, HYLDA Technical Report 70, January 2000.
7. Bippes, H., Instability Features Appearing on SweptWing Configurations. In: Laminar- Turbulent Transition. IUTAM Symposium Toulouse/France, September 11-15, 1989, Springer-Verlag, Berlin/Heidelberg/New York, 1990,.
8. Deyhle, H., Bippes, H., Disturbance growth in an unstable three-dimensional boundary layer and its dependence on environmental conditions. JFM 316 (1996), 73-113.
9. Abegg, C., Bippes, H., Bertolotti, F. P., On the Application of Suction for the Stabilization of Crossflow Instability over Perforated Walls. In: W. Nitsche, H.J. Heinemann, R. Hilbig, New Results in Numerical and Experimental Fluid Mechanics II, Contributions to the 11th AG STAB/DGLR Symposium Berlin, Germany 1998, pp 1.
10. W. Pfenninger, Some results from the X-21 program. Part I: Flow phenomena at the leading edge of swept wings. In: Recent developments in boundary layer research Part IV, AGARDograf 97, May 1965.
11. D.I.A Poll Some Observations of the Transition Process on theWindward Face of a Long Yawed Cylinder, J. Fluid Mech., 150, 329-356 (1985).
12. G. Schrauf Transition Prediction Using Different Linear Stability Analysis Strategies, AIAA-Paper 94-1848, 12th AIAA Applied Aerodynamics Conference, Colorado Springs, CO, USA, June 1994. pp. 367-375.
13. J. Archambaud HYLDA Technical Report 74, in preparation.