scholarly journals Interaction of a pair of vortex wakes at Mach 3

2021 ◽  
Author(s):  
A. S. Shmakov ◽  
A. M. Shevchenko
Keyword(s):  
Mach 3

scholarly journals Developement of 3D printer for silicate-based materials

2020 ◽  
Vol 2 (SI2) ◽  
pp. First
Author(s):  
Can Chi Trieu ◽  
Minh-Thien Nguyen ◽  
Thien-Toan Quan Le ◽  
Manh-Quyen Dam ◽  
Anh-Tu Tran ◽  
...  
Keyword(s):  
3D Printing ◽  
Manufacturing Industry ◽  
3D Printer ◽  
Printing Technology ◽  
3D Printing Technology ◽  
Frame Element ◽  
Key Factor ◽  
Stepper Motors ◽  
Mach 3 ◽  
Near Future

3D printer and 3D printing technology are now considered as one of the key factor in the manufacturing industry. In the near future, we could envisage different application of 3D printing method in the sector of materials processing and production. In the sector of civil engineering, they existed somewhere some construction works developed with 3D printing technology.  In this study, we aim to manufacture laboratory-scale printers with nozzles and extrusion feeding systems suitable for paste such as the case of clay-based materials of silicate industry. The movement system was encoded and controlled via the motherboard (Mach 3 controller software). Stepper motors and shaft drives were also implemented in the frame element of such printer. The feeding system was designed based on the extrusion method including cylinder and piston element. Based on that, sample size 200x300x300mm was available for operation testing. Concerning the performance of the instrument, we have obtained printed specimens with different geometric shapes with complexity. From the obtained result, we also discussion on the feasibility up scaling the study and developing a 3D printer for silicate based materials.

Heat Transfer and Pressure Distribution in Open Cavity Flow

1967 ◽  
Vol 89 (1) ◽  
pp. 103-108 ◽  
Author(s):  
A. F. Emery ◽  
J. A. Sadunas ◽  
M. Loll
Keyword(s):  
Heat Transfer ◽  
Pressure Distribution ◽  
Flat Plate ◽  
Cavity Flow ◽  
Rectangular Cavity ◽  
Open Cavity ◽  
Transfer Coefficients ◽  
Transient Techniques ◽  
Heat Transfer Coefficients ◽  
Mach 3

The heat transfer and pressure distribution in a rectangular cavity in a Mach 3 flow were investigated for a rectangular and an inverted-wedge recompression step. Noticeable differences between the results for the two steps were found in the recovery factors, but no real differences were detected in the heat-transfer coefficients or the velocity profiles. Heat-transfer coefficients in the cavity were determined by transient techniques and were found to range from 50 to 110 percent of the flat-plate value just prior to the expansion step.

Longitudinal Aerodynamics of a Canard Guided Spin Stabilized Projectile

2012 ◽  
Vol 443-444 ◽  
pp. 719-723
Author(s):  
Xiu Ling Ji ◽  
Hai Peng Wang ◽  
Shi Ming Zeng ◽  
Chen Yang Jia
Keyword(s):  
Normal Force ◽  
Navier Stokes ◽  
Test Case ◽  
Aerodynamic Coefficients ◽  
Number Range ◽  
Detailed Understanding ◽  
Pitch Moment ◽  
Spinning Projectile ◽  
Mach 3 ◽  
Viable Approach

Navier–Stokes simulation is performed on a canard guided spinning projectile for different attack angles and circumferential position angles of canard over the Mach number range of 1.8–2.2. The computational Magnus moment coefficients of test case are validated with available experimental data of a Secant-Ogive-Cylinder-Boattail (SOCBT) configuration at Mach 3, demonstrating that the method can provide an accurate and viable approach for this problem. The aim of the present study is to provide a detailed understanding of the effects of canard with different circumferential position angles on longitudinal aerodynamic coefficients at three supersonic speeds and various angles of attack. And the results show that normal force coefficients and pitch moment coefficients vary periodically with the circumferential position angles of canard.

Computational study of the cavity flow over sharp nose cone in supersonic flow

2020 ◽  
Vol 31 (06) ◽  
pp. 2050079 ◽  
Author(s):  
F. Pish ◽  
Tran Dinh Manh ◽  
M. Barzegar Gerdroodbary ◽  
Nguyen Dang Nam ◽  
Rasoul Moradi ◽  
...  
Keyword(s):  
Computational Study ◽  
Fluid Dynamic ◽  
Thermal Characteristic ◽  
Main Body ◽  
Cavity Depth ◽  
Nose Cone ◽  
Sst Turbulence Model ◽  
Mach 3 ◽  
Cfd Method ◽  
Supersonic Vehicles

Heat and drag reduction on the nose cone is a significant issue for increasing the speed of the supersonic vehicles. In this paper, computational fluid dynamic method is applied to investigate the thermal and drag coefficient on the sharp nose cone with different cavity shapes. In order to simulate our model, the CFD method with SST turbulence model is applied to study the flow feature and temperature distribution in the vicinity of the nose body. The effect of depth and length of the cavity on the thermal characteristic of the nose cone is comprehensively investigated. In addition, the influence of the number of the cavity in the thermal performance of the main body is studied. According to our results, increasing the length of the cavity highly efficient for the reduction of the drag at Mach = 3. As the Mach number is increased to 3, the number of the cavity becomes a significant role and it is observed that case 9 with four cavities is more efficient. Obtained results also show that increasing the cavity depth declines the temperature on the main body. Our findings confirm that the main source of the expansion is the edge of the cavity.

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