Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform

Volume: 19 Number: 1 May 10, 2016
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Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform

Abstract

The present experimental work investigates the near surface flow structure and aerodynamic characteristics of X-45 type non-slender delta wing planform using dye visualization, Stereoscopic Particle Image Velocimetry (stereo-PIV) and aerodynamic load measurements. The instantaneous images are acquired on the plan-view plane within 5o a ≤ 20o to calculate the time-averaged flow data.  In order to compare flow structures with other non-slender wing planforms such as delta and lambda, previously presented dye visualization and stereo-PIV results are also provided. It can be concluded that vortical flow with a pair of well-defined LEVs over X-45 develop at very low angles of attack, and form close to the wing surface similar to delta and lambda planforms. The stall occurs at an angle of attack a = 32o, whereas stalling is evident at relatively lower angles of attack for simple delta wing.

Keywords

References

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Details

Primary Language

English

Subjects

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Journal Section

-

Publication Date

May 10, 2016

Submission Date

February 3, 2016

Acceptance Date

-

Published in Issue

Year 2016 Volume: 19 Number: 1

APA
Yanıktepe, B., Özalp, C., & Canpolat, Ç. (2016). Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform. Kahramanmaraş Sütçü İmam Üniversitesi Mühendislik Bilimleri Dergisi, 19(1), 1-10. https://doi.org/10.17780/ksujes.86852

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