Use of empirical transition correlations for flow around high-lift configurations

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Bertelrud, Arild ^a  

^a ANALYTICAL SERVICES AND MATERIALS INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING;

EXPERIMENTAL DATABASE; HIGH LIFTS; NAVIER-STOKES CODE; TRANSITION CRITERION;

NAVIER STOKES EQUATIONS;

EID: 84983146154     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-541     Document Type: Conference Paper

References (14)

1. Bertelrud, A. “Transition on a three-element high lift configuration at high Reynolds numbérs.” AIAA Paper 98-0703 presented at the AIAA Aerospace Sciences Conference, RencvNV, January 12-15, 1998.
2. Bertelrud, A., Johnson, S., Lytle, C. and Mills, P.: “A System for Analysis of Transition Characteristics on a High-Lift Configuration at High Reynolds Numbers.” presented at thel7th ICIASF, Sept 29 - Oct 2, 1997, Monterey.CA.
3. Rurhsey, C.L., Gatski, T.B., Ying, S X. and Bertelrud, A.: “Prediction of High-Lift Flows UsingTurbulent Closure Models.” AIAA Paper 7-2260, 15th AIAA Applied Aerodyn. Conf, June 23-25, 1997 Atlanta, GA.
4. White F M.: “Viscous Fluid Flow.” McGraw-Hill, New York, 1974.
5. Abu-Ghannam, B.J. and Shaw, R.: “Natural transition of boundary layers - the effects of turbuíence pressure gradient, and flow history.” J. Mech Eng Sei, Vol.22, No 5, 213-228 (1980)
6. Narasimha, R.: “On the distribution of interrriittency in the transition region of a boundary layer.” J. Aeronaut. Sei. Vol 224, 711-712 (1957)
7. Horton, H.P.: “A semi-empirical theory for the growth and bursting of laminar separation bubbles.” ARC CP-1073 (1969)
8. Roberts, W.B.: “Calculation of laminar separation bubbles.” J Aircraft, Vol. 18, No. 1, 1980
9. Michel, R.: “Détermination du Point de Transition of Calcul de la Trainéee des profils d'Ailes en incompressible.” La Recherche Aéronautique, No 24 (1951)
10. Granville, P. S.: “The calculation of viscous drag of bodies of revolution.” Navy Department. The David Taylor Model Basin. Report, No. 849, 1953.
11. van Driest, E.R. and Blumer, C.B.: “Boundary Layer Transition Freestream and Pressure Gradient Effects.” AIAA Journal, Vol. 1, No. 6 (June 1963)
12. Wazzan, A.R., Gazleyjr, C. and Smith, A.M.O. “H-Rx method for predicting transition.” AIAA Vol. 19, No 6, 810-812 (1981)
13. Drela, M. and Giles M.B. “Viscous-inviscid analysis of transonic and low Reynolds number airfoils.” AIAA Journal, Vol. 25, No. 10, 1347-1355, (1987)
14. Govindarajan, R. and Narasimha, R.: “The role of residual non-turbulent disturbances on transition onset in two-dimensional boundary layers.” J. Fluids Eng. (1990)