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Information Seminar Paper

Title

3D SIMULATION AND ANALYSIS OF CROPPED DELTA WING VORTEX

Pages

  -

Abstract

 SIMULATION OF VORTEX STRUCTURES AND STUDYING THEIR EFFECTS ON THE PERFORMANCE FACTORS, IS ONE OF THE MOST DEMANDING STAGES IN THE AERODYNAMIC DESIGN OF FLIGHT VEHICLES. THESE CHAOTIC FLOW PATTERNS ARE MORE IMPORTANT FOR HIGH MANEUVER DELTA WING AIRCRAFTS WHERE THE HIGH ATTACK ANGLES ARE UNAVOIDABLE. IN SUCH CONDITIONS A LONGITUDINAL VORTEX IS ALWAYS OBSERVED ON TOP OF THE LEADING EDGE AND PLAYS A VERY IMPORTANT ROLE IN AERODYNAMIC PERFORMANCE SHIFTS AND STABILITY OF FLIGHT VEHICLE. IN THIS PAPER, THE RESULTS OF HIGHLY ACCURATE THREE DIMENSIONAL NUMERICAL SIMULATION OF CROPPED DELTA WING FOR INVESTIGATING THE VORTEX BEHAVIOR, HAS BEEN PRESENTED. FOR THIS STUDY THE NAVIER-STOCKS EQUATIONS HAVE BEEN SOLVED BY 24 COMPUTATIONAL NODES OF CLUSTER COMPUTER, IN A 3D STRUCTURAL GRID DOMAINS.

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  • Cite

    APA: Copy

    Sahebi, Eiman B., Ranjbari, MohamadReza, Sharifzadeh, Soheil, & Gouping, H.. (2015). 3D SIMULATION AND ANALYSIS OF CROPPED DELTA WING VORTEX. CONFERENCE OF IRANIAN AEROSPACE SOCIETY. SID. https://sid.ir/paper/945714/en

    Vancouver: Copy

    Sahebi Eiman B., Ranjbari MohamadReza, Sharifzadeh Soheil, Gouping H.. 3D SIMULATION AND ANALYSIS OF CROPPED DELTA WING VORTEX. 2015. Available from: https://sid.ir/paper/945714/en

    IEEE: Copy

    Eiman B. Sahebi, MohamadReza Ranjbari, Soheil Sharifzadeh, and H. Gouping, “3D SIMULATION AND ANALYSIS OF CROPPED DELTA WING VORTEX,” presented at the CONFERENCE OF IRANIAN AEROSPACE SOCIETY. 2015, [Online]. Available: https://sid.ir/paper/945714/en

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