X-45 Tipi Delta Kanat Modeli Üzerinde Oluşan Akış Karakteristikleri ve Aerodinamiği

Cilt: 19 Sayı: 1 10 Mayıs 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

Kaynakça

  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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  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.
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Ayrıntılar

Birincil Dil

İngilizce

Konular

-

Bölüm

-

Yayımlanma Tarihi

10 Mayıs 2016

Gönderilme Tarihi

3 Şubat 2016

Kabul Tarihi

-

Yayımlandığı Sayı

Yıl 1970 Cilt: 19 Sayı: 1

Kaynak Göster

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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