Numerical Study of Aerodynamics and Flow Physics of the 30P30N Three-Element Airfoil in Dynamic Ground Effect

2016 ◽  
Author(s):  
Qiulin Qu ◽  
Liewei Huang ◽  
Peiqing Liu ◽  
Wei Wang ◽  
Ramesh K. Agarwal
Keyword(s):  
Numerical Study ◽  
Ground Effect ◽  
Flow Physics

Numerical Study on Aerodynamics and Flow Physics of a Flapping Wing Hovering in Ground Effect

2019 ◽  
Author(s):  
Qiulin Qu ◽  
Lianchao Xu ◽  
Peiqing Liu ◽  
Yunlong Zheng ◽  
Ramesh K. Agarwal
Keyword(s):  
Numerical Study ◽  
Ground Effect ◽  
Flapping Wing ◽  
Flow Physics

Numerical study of the aerodynamics of a NACA 4412 airfoil in dynamic ground effect

2014 ◽  
Vol 38 ◽  
pp. 56-63 ◽  
Author(s):  
Qiulin Qu ◽  
Xi Jia ◽  
Wei Wang ◽  
Peiqing Liu ◽  
Ramesh K. Agarwal
Keyword(s):  
Numerical Study ◽  
Ground Effect

Numerical Investigation on Turbulence Statistics and Heat Transfer of a Circular Jet Impinging on a Roughened Flat Plate

2021 ◽  
Vol 13 (4) ◽  
Author(s):  
Abdulrahman Alenezi ◽  
Abdulrahman Almutairi ◽  
Hamad Alhajeri ◽  
Abdulaziz Gamil ◽  
Faisal Alshammari
Keyword(s):  
Heat Transfer ◽  
Reynolds Number ◽  
Numerical Study ◽  
Roughness Element ◽  
Three Dimensional ◽  
Reynolds Numbers ◽  
Target Plate ◽  
Cross Sectional ◽  
Flow Physics ◽  
Baseline Case

Abstract A detailed heat transfer numerical study of a three-dimensional impinging jet on a roughened isothermal surface is presented and is investigated from flow physics vantage point under the influence of different parameters. The effects of the Reynolds number, roughness location, and roughness dimension on the flow physics and heat transfer parameters are studied. Additionally, the relations between average heat transfer coefficient (AHTC) and flow physics including pressure, wall shear and flow vortices with thermodynamic nonequilibrium are offered. This paper studies the effect of varying both location and dimension of the roughness element which took the shape of square cross-sectional continuous ribs to deliver a favorable trade-off between total pressure loss and heat transfer rate. The roughness element was tested for three different radial locations (R/D) = 1, 1.5, and 2 and at each location its height (i.e., width) (e) was changed from 0.25 to 1 mm in incremental steps of 0.25. The study used a jet angle (α) of 90 deg, jet-to-target distance (H/D = 6), and Re ranges from 10,000 to 50,000, where H is the vertical distance between the target plate and jet exit. The results show that the AHTC can be significantly affected by changing the geometry and dimensions of the roughness element. This variation can be either an augmentation of, or decrease in, the (HTC) when compared with the baseline case. An enhancement of 12.9% in the AHTC was achieved by using optimal location and dimensions of the roughness element at specific Reynolds number. However, a diminution between 10% and 30% in (AHTC) was attained by the use of rib height e = 1 mm at Re = 50k. The variation of both rib location and height showed better contribution in increasing heat transfer for low-range Reynolds numbers.

scholarly journals Numerical study of flow around NACA0015 in ground effect

2016 ◽  
Vol 114 ◽  
pp. 02069
Author(s):  
Khadidja Malti ◽  
Hanaa Hebow ◽  
Bachir Imine
Keyword(s):  
Numerical Study ◽  
Ground Effect

Numerical Study of Aerodynamics of a Wing-in-Ground-Effect Craft

2014 ◽  
Vol 51 (3) ◽  
pp. 913-924 ◽  
Author(s):  
Qiulin Qu ◽  
Zhe Lu ◽  
Peiqing Liu ◽  
Ramesh K. Agarwal
Keyword(s):  
Numerical Study ◽  
Ground Effect ◽  
Wing In Ground Effect

DDES study of the aerodynamic forces and flow physics of a delta wing in static ground effect

2015 ◽  
Vol 43 ◽  
pp. 423-436 ◽  
Author(s):  
Yunpeng Qin ◽  
Qiulin Qu ◽  
Peiqing Liu ◽  
Yun Tian ◽  
Zhe Lu
Keyword(s):  
Delta Wing ◽  
Ground Effect ◽  
Aerodynamic Forces ◽  
Flow Physics
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