Click for new scientific resources and news about Corona[COVID-19]

Paper Information

Journal:   FLUID MECHANICS AND AERODYNAMICS JOURNAL   SPRING-SUMMER 2017 , Volume 5 , Number 1 ; Page(s) 1 To 15.
 
Paper: 

NUMERICAL INVESTIGATION OF AEROACOUSTIC PHENOMENON FLOW OVER TAILLESS, DOUBLE, AND DIAMOND DELTA WINGS, USING LARGE EDDY SIMULATION

 
 
Author(s):  RAMEZANIZADEH M.*, MOHAMMADI H.
 
* AEROSPACE ENGINEERING DEPARTMENT, SHAHID SATTARI AERONAUTICAL UNIVERSITY OF SCIENCE & TECHNOLOGY
 
Abstract: 

The objective of this paper is to obtain acoustical behavior of flow around 50° tailless, 80°/65° double and 53° diamond delta wing configurations, using large eddy simulation. Validation of the aerodynamic coefficients is performed using available experimental results, showing good agreements. CFD simulations were performed for 15 degree angles of attack at a Mach number of 0.147 and a Reynolds number of 1.2 million, based on the root chord root chord of the wings (is 360 mm). Acoustic measurements, such as power spectral density, acoustic pressure, sound pressure level, and sound amplitude were taken, using 3 microphones in the wake region of the mentioned wings. The amount of sound pressure level of microphone, which is placed at 1.835 meter from apex of above wings in DK Strouhal number 0 to 1 is, 24 to 69, 10 to 54 and 9 to 44. Hence, for purposes of being silence, aeroacoustics values indicate that diamond delta wing is more preferable than tailless and double delta wing.

 
Keyword(s): AEROACOUSTICS, DIAMOND DELTA WING, SOUND PRESSURE LEVEL, VORTEX INTERACTIONS, LARGE EDDY SIMULATION APPROACH, STROUHAL NUMBER
 
 
References: 
  • Not Registered.
  •  
 
+ Click to Cite.
APA: Copy

RAMEZANIZADEH, M., & MOHAMMADI, H. (2017). NUMERICAL INVESTIGATION OF AEROACOUSTIC PHENOMENON FLOW OVER TAILLESS, DOUBLE, AND DIAMOND DELTA WINGS, USING LARGE EDDY SIMULATION. FLUID MECHANICS AND AERODYNAMICS JOURNAL, 5(1 ), 1-15. https://www.sid.ir/en/journal/ViewPaper.aspx?id=568976



Vancouver: Copy

RAMEZANIZADEH M., MOHAMMADI H.. NUMERICAL INVESTIGATION OF AEROACOUSTIC PHENOMENON FLOW OVER TAILLESS, DOUBLE, AND DIAMOND DELTA WINGS, USING LARGE EDDY SIMULATION. FLUID MECHANICS AND AERODYNAMICS JOURNAL. 2017 [cited 2021May16];5(1 ):1-15. Available from: https://www.sid.ir/en/journal/ViewPaper.aspx?id=568976



IEEE: Copy

RAMEZANIZADEH, M., MOHAMMADI, H., 2017. NUMERICAL INVESTIGATION OF AEROACOUSTIC PHENOMENON FLOW OVER TAILLESS, DOUBLE, AND DIAMOND DELTA WINGS, USING LARGE EDDY SIMULATION. FLUID MECHANICS AND AERODYNAMICS JOURNAL, [online] 5(1 ), pp.1-15. Available: https://www.sid.ir/en/journal/ViewPaper.aspx?id=568976.



 
 
Persian Abstract Yearly Visit 40
 
Latest on Blog
Enter SID Blog