- Видео 15
- Просмотров 504
Dhananjay Bodas
Добавлен 2 дек 2015
Welcome to Engineering - Your Home for Applied Science Mastery
Dive into the fascinating world of applied science with specifically tailored educational tutorials that empower, educate, and inspire. At Engineering, we are dedicated to unlocking the complexities of engineering using cutting-edge software like ANSYS 2020R1, Hypermesh 2019, Hypergraph 2019, and LS-DYNA.
🔍 What to Expect:
Step-by-Step Guides: Follow along with in-depth tutorials that take you from novice to expert in no time
Software Mastery: Get hands-on with ANSYS for simulation tasks, Hypermesh for preprocessing, Hypergraph for postprocessing, and LS-DYNA for dynamic analysis.
Real-World Applications: See theory put into practice with scenarios that showcase how applied science is pivotal in solving engineering problems.
source for advanced educational content in applied science.
Let's engineer our way to innovation and deep understanding. Start learning with us today!
Dive into the fascinating world of applied science with specifically tailored educational tutorials that empower, educate, and inspire. At Engineering, we are dedicated to unlocking the complexities of engineering using cutting-edge software like ANSYS 2020R1, Hypermesh 2019, Hypergraph 2019, and LS-DYNA.
🔍 What to Expect:
Step-by-Step Guides: Follow along with in-depth tutorials that take you from novice to expert in no time
Software Mastery: Get hands-on with ANSYS for simulation tasks, Hypermesh for preprocessing, Hypergraph for postprocessing, and LS-DYNA for dynamic analysis.
Real-World Applications: See theory put into practice with scenarios that showcase how applied science is pivotal in solving engineering problems.
source for advanced educational content in applied science.
Let's engineer our way to innovation and deep understanding. Start learning with us today!
NACA 64 008
6 Digit Un symmetrical airfoil with a 0-degree angle of attack and L=300mm
r=30mm
Airfoil was subtracted from the fluid domain using boolean operation
Detached eddy simulation and RANS model was Relizable k-epsilon
Dragccoffiont airfoil 4.1213957e-28
Drag force airfoil 2.5243549e-28 N
Lift Cofficient airfoil 7.5833682e-27
Lift Focre airfoil 4.644813e-27 N
Monent Cofficien airfoil 2.0639177e-28
Moment airfoil 1.2641496e-28N-M
Force airfoil X 2.5243549e-28 N
Force on airfoil Y221.068 N
Minimum Value of Pressure on airfoil-19088.7 Pa
Maximum Value of Pressure on airfoil 33136.9 Pa
r=30mm
Airfoil was subtracted from the fluid domain using boolean operation
Detached eddy simulation and RANS model was Relizable k-epsilon
Dragccoffiont airfoil 4.1213957e-28
Drag force airfoil 2.5243549e-28 N
Lift Cofficient airfoil 7.5833682e-27
Lift Focre airfoil 4.644813e-27 N
Monent Cofficien airfoil 2.0639177e-28
Moment airfoil 1.2641496e-28N-M
Force airfoil X 2.5243549e-28 N
Force on airfoil Y221.068 N
Minimum Value of Pressure on airfoil-19088.7 Pa
Maximum Value of Pressure on airfoil 33136.9 Pa
Просмотров: 3
Видео
NACA 6049
Просмотров 8Месяц назад
Scale adaptivity simulation with k-omega convergence since density is constant throughout the fluid domain so the flow is pressure-based Drag=262.5746 Drag force=1608208N lift=232.5627 Lift force=1425.5627N Moment=116.8019N-M Moment force=71.54129N-M force=160.8208N
ANSYS 2020 R1
Просмотров 30Месяц назад
NACA 1410 is 4 digit airfoil that was used with RANS (Reynoid average shear stress) convergence Gemotrycrenctinwas R=30mm and L=300mm with fluid domain the boolean operation was used to subtract airfoil NACA 4-digit airfoil specification This NACA airfoil series is controlled by 4 digits e.g. NACA 2412, which designate the camber, position of the maximum camber, and thickness. If an airfoil num...
Vortex Generator
Просмотров 3Месяц назад
Vortex Generator in ANSYS 2020R1 2D gemmetry was used boundary condition's are- 1 inlet velocity =100m\s 2 Outlet presure=0bar So flow is density based Finnite difference method was used to calculate results
4 Adams View Adams 2020 Slider crank mechanism
Просмотров 122 месяца назад
Slider crank mechanism inversion 3 INVERSION: We have already discussed that when one of the links is fixed in a kinematic chain, it is called a mechanism. So we can obtain as many mechanisms as the number of links in a kinematic chain by fixing, in turn, different links in a kinematic chain. This method of obtaining different mechanisms by fixing different links in a kinematic chain is known a...
3 Adams View Adams 2020
Просмотров 472 месяца назад
Slider crank mechanism inversion 2 Whitworth Quick Returns Mechanism: In this mechanism, the fixed crank is used to convert rotary motion into oscillating motion.
2 Adams View Adams 2020
Просмотров 312 месяца назад
Slider crank mechanism inversion 1 Reciprocating engines: In internal combustion engines, the first inversion of the slider crank mechanism is used to convert the rotary motion of the crankshaft into the reciprocating motion of the piston. Reciprocating compressors: Similar to reciprocating engines, the first inversion is employed in compressors to convert rotary motion into linear motion, comp...
1 Adams View Adams 2020 Slider crank mechanism
Просмотров 322 месяца назад
Slider crank mechanism with no inversion
NACA 2412wmv
Просмотров 612 месяца назад
k-epsilon converges were used Fluid domain with radius =30 mm length= 300mm 2D was used using boolean airfoil was subtracted Transient behavior using with hybrid initialization Solver is pressure-based Force on airfoil X-axis 188.035 [N] Torque on airfoil Z-axis 23.4458 [N m]
NACA 2412
Просмотров 1342 месяца назад
k-omega converges were used Fluid domain with radius =30 mm length= 300mm 2D was used using boolean airfoil was subtracted Transient behavior using hybrid initialization Force on airfoil 207.573 [N] Torque on airfoil Z-axis 19.7482 [N m]
NACA 009
Просмотров 892 месяца назад
NACA 009 converges were used Fluid domain with radius =30 mm length= 300mm 2D was used using boolean airfoil was subtracted Transient behavior using with hybrid initialization
RANS(Reynold Average shear stress)
Просмотров 183 месяца назад
RANS converges were used Fluid domain with radius =30 mm length= 300mm 2D was used using boolean airfoil was subtracted Transient behavior using with hybrid initialization
Inviscous flow
Просмотров 203 месяца назад
4digit non-symmetrical airfoil with 0-degree angle of attack 2-D fluid domain with the use of boolean subtract from fluid domain to airfoil
NACA 006
Просмотров 96 месяцев назад
Symmetrical airfoil with input velocity =100m/s Outlet pressure=0Pa Mach number=1.76 so follow is subsonic pressure driven flow constant density=1.25kg/mm^3 Hybrid initiation