Computational Investigation of A Blended Wing Body at Low Speeds-Reference-Cited by-同舟云学术

Computational Investigation of A Blended Wing Body at Low Speeds

Published:2023-07-25 Issue: Volume: Page:147-155
ISSN:0972-950X
Container-title:Journal of Aerospace Sciences and Technologies
language:
Short-container-title:joast

Author:

Mohan Shuvendra,Kumar Priyank

Abstract

Experiments and computations were made on a blended wing body at a free stream velocity of 18 m/s and at different AoA. Experiments consisted of flow visualizations using oil and tuft flow techniques. Computations were made using the commercial software ANSYS Fluent. Results indicated a highly complex flow behavior in the leeward side of the blended wing body. Reasonable agreement between experiments and computations was observed.

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