NUMERICAL INVESTIGATION OF TRANSONIC TURBULENT FLOW OVER ONERA M6 WING

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EBRAHIMI MOSTAFA; Noori Sahar; Ajalli Fariba

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Seminar Paper

Paper Information

Seminar: CONFERENCE OF IRANIAN AEROSPACE SOCIETY
Year:2015 | Issue:14

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Title

NUMERICAL INVESTIGATION OF TRANSONIC TURBULENT FLOW OVER ONERA M6 WING

Author(s)

EBRAHIMI MOSTAFA | Noori Sahar | Ajalli Fariba

Keywords

CFD

ONERA M6

SPALART- ALLMARAS

WING

Abstract

THIS CASE INVOLVES THE FLOW OVER THE ONERA M6 WING. IT WAS TESTED IN A WIND TUNNEL AT TRANSONIC MACH NUMBERS 0.8395 AND ANGLES-OF-ATTACK 3.06 DEGREE. THE REYNOLDS NUMBERS WERE ABOUT 12 MILLION BASED ON THE MEAN AERODYNAMIC CHORD. THE ONERA M6 WING IS A CLASSIC CFD VALIDATION CASE FOR EXTERNAL FLOWS BECAUSE OF ITS SIMPLE GEOMETRY COMBINED WITH COMPLEXITIES OF TRANSONIC FLOW (I.E. LOCAL SUPERSONIC FLOW, SHOCKS, AND TURBULENT BOUNDARY LAYERS SEPARATION). THE ONERA M6 WING IS A WELL-KNOWN REFERENCE USED TO VALIDATE CFD METHODS IN THE TRANSONIC DOMAIN, ONE OF THE AREAS THAT THE FLUID DYNAMICS HAD A LARGE IMPACT IN ONERA M6.THE ONERA-M6 WING IS A WIDELY USED THREE-DIMENSIONAL TEST CASE FOR THE VALIDATION OF NUMERICAL METHODS AND TURBULENT MODELS, THE PERFORMANCE OF ANY AIRBORNE VEHICLE LARGELY DEPENDS ON ITS WING DESIGN.

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APA: Copy

EBRAHIMI, MOSTAFA, Noori, Sahar, & Ajalli, Fariba. (2015). NUMERICAL INVESTIGATION OF TRANSONIC TURBULENT FLOW OVER ONERA M6 WING. CONFERENCE OF IRANIAN AEROSPACE SOCIETY. SID. https://sid.ir/paper/945697/en

Vancouver: Copy

EBRAHIMI MOSTAFA, Noori Sahar, Ajalli Fariba. NUMERICAL INVESTIGATION OF TRANSONIC TURBULENT FLOW OVER ONERA M6 WING. 2015. Available from: https://sid.ir/paper/945697/en

IEEE: Copy

MOSTAFA EBRAHIMI, Sahar Noori, and Fariba Ajalli, “NUMERICAL INVESTIGATION OF TRANSONIC TURBULENT FLOW OVER ONERA M6 WING,” presented at the CONFERENCE OF IRANIAN AEROSPACE SOCIETY. 2015, [Online]. Available: https://sid.ir/paper/945697/en

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