Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
Modern day fighter aircrafts are mostly canard configured because of its advantages over conventional configuration. The primary objective of this work is to investigate the low speed aerodynamic and stability characteristics of a canard configured aircraft. Using CFD -ANSYS Fluent package, numeric...
محفوظ في:
| المؤلفون الرئيسيون: | , |
|---|---|
| التنسيق: | مقال |
| اللغة: | English English |
| منشور في: |
Penerbit Akademia Baru
2019
|
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://irep.iium.edu.my/68505/1/68505_Experimental%20and%20numerical%20study.pdf http://irep.iium.edu.my/68505/2/68505_Experimental%20and%20numerical%20study_SCOPUS.pdf http://irep.iium.edu.my/68505/ http://www.akademiabaru.com/doc/ARFMTSV53_N2_P165_174.pdf |
| الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
| الملخص: | Modern day fighter aircrafts are mostly canard configured because of its advantages over conventional configuration. The primary objective of this work is to investigate the low speed aerodynamic and stability characteristics of a canard configured aircraft. Using CFD -ANSYS Fluent package, numerical flow simulations were carried out for a typical canard configuration such as Burt Rutan’s VariEze, a composite homebuilt canard aircraft. To validate the numerical results, wind tunnel testing of a scaled model was carried out. Finally the effect of horizontal location of canard on the aerodynamics and stability characteristics was studied. |
|---|