Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform

Volume: 19 Number: 1 May 10, 2016
EN TR

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

  1. [1]. Gursul I., Gordinier R., and Visbal M. (2005). “Unsteady Aerodynamics of Nonslender Delta Wings” Progress in Aerospace Sciences Vol.41, pp.515-557.
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  4. [4]. Canpolat C., Yayla, S., Sahin, B., and Akilli, H. (2009). “Dye Visualization of the Flow Structure over a Yawed Nonslender Delta Wing”, Journal of Aircraft ,Vol. 46, No. 5.
  5. [5]. Sahin B, Yayla S, Canpolat C, and Akilli H. (2012) "Flow structure over the yawed nonslender diamond wing", Aerospace Science and Technology, vol. 23, no. 1, pp. 108-119.
  6. [6]. Cui, Y. D. , Lim T. T., Tsai H. M., (2007) “Control of Vortex Breakdown over a Delta Wing Using Forebody Slot Blowing”, AIAA Journal, Vol. 45, No. 1., pp. 110-117.
  7. [7]. Menke, M., Yang, H., and Gursul, I., (1999). “Experiments on the Unsteady Nature of Vortex Breakdown over Delta Wings”, Experiments in Fluids, Vol. 27, pp. 262-272.
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Details

Primary Language

English

Subjects

-

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
AMA
1.Yanıktepe B, Özalp C, Canpolat Ç. Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform. KSU J. Eng. Sci. 2016;19(1):1-10. doi:10.17780/ksujes.86852
Chicago
Yanıktepe, Bülent, Coşkun Özalp, and Çetin Canpolat. 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.
EndNote
Yanıktepe B, Özalp C, Canpolat Ç (May 1, 2016) Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform. Kahramanmaraş Sütçü İmam Üniversitesi Mühendislik Bilimleri Dergisi 19 1 1–10.
IEEE
[1]B. Yanıktepe, C. Özalp, and Ç. Canpolat, “Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform”, KSU J. Eng. Sci., vol. 19, no. 1, pp. 1–10, May 2016, doi: 10.17780/ksujes.86852.
ISNAD
Yanıktepe, Bülent - Özalp, Coşkun - Canpolat, Çetin. “Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform”. Kahramanmaraş Sütçü İmam Üniversitesi Mühendislik Bilimleri Dergisi 19/1 (May 1, 2016): 1-10. https://doi.org/10.17780/ksujes.86852.
JAMA
1.Yanıktepe B, Özalp C, Canpolat Ç. Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform. KSU J. Eng. Sci. 2016;19:1–10.
MLA
Yanıktepe, Bülent, et al. “Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform”. Kahramanmaraş Sütçü İmam Üniversitesi Mühendislik Bilimleri Dergisi, vol. 19, no. 1, May 2016, pp. 1-10, doi:10.17780/ksujes.86852.
Vancouver
1.Bülent Yanıktepe, Coşkun Özalp, Çetin Canpolat. Aerodynamics and Flow Characteristics of X-45 Delta Wing Planform. KSU J. Eng. Sci. 2016 May 1;19(1):1-10. doi:10.17780/ksujes.86852

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