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AJAY SAMPATH H A
India
เข้าร่วมเมื่อ 31 มี.ค. 2020
วีดีโอ
Sandwich rectangular cantilever beam - Ansys APDL
มุมมอง 2.7K3 ปีที่แล้ว
Sandwich rectangular cantilever beam - Ansys APDL
Tapered flat plate with hole in the center & Vertical loading Ansys APLD
มุมมอง 5363 ปีที่แล้ว
Tapered flat plate with hole in the center & Vertical loading Ansys APLD
Flat plate fixed at one end, a hole in the center & load applied on vertical direction - ANSYS APLD
มุมมอง 5033 ปีที่แล้ว
Flat plate fixed at one end, a hole in the center & load applied on vertical direction - ANSYS APLD
Exp 2 : Compressible and viscous flow over airfoil velocity vectors for subsonic
มุมมอง 1.1K3 ปีที่แล้ว
Exp 2 : Compressible and viscous flow over airfoil velocity vectors for subsonic
Exp 1 Modeling of Symmetric Cambered Aerofoil Geometry + Generation of Body Fitting Adaptive Mesh
มุมมอง 3.5K3 ปีที่แล้ว
Exp 1 Modeling of Symmetric Cambered Aerofoil Geometry Generation of Body Fitting Adaptive Mesh
Exp: 5 Isentropic flow analysis in a 2D supersonic diffuser and asupersonic nozzle.
มุมมอง 6543 ปีที่แล้ว
Exp: 5 Isentropic flow analysis in a 2D supersonic diffuser and asupersonic nozzle.
Exp - 4 Isentropic flow analysis in a 2D subsonic diffuser and asubsonic nozzle.
มุมมอง 1.1K3 ปีที่แล้ว
Exp - 4 Isentropic flow analysis in a 2D subsonic diffuser and asubsonic nozzle.
Axial Flow Compressors - Velocity Triangles - Performance Parameters
มุมมอง 1.1K4 ปีที่แล้ว
Axial Flow Compressors - Velocity Triangles - Performance Parameters
Turbines - Introduction - Cooling Techniques
มุมมอง 764 ปีที่แล้ว
Turbines - Introduction - Cooling Techniques
Axial Compressor Introduction - Velocity Diagram
มุมมอง 4364 ปีที่แล้ว
Axial Compressor Introduction - Velocity Diagram
Inlets - Module 3 - Minimum area derivation
มุมมอง 5414 ปีที่แล้ว
Inlets - Module 3 - Minimum area derivation
Centrifugal Compressor - Working and Velocity Triangles
มุมมอง 1244 ปีที่แล้ว
Centrifugal Compressor - Working and Velocity Triangles
03 Propeller part design (Propeller Hub - Assembly)
มุมมอง 1.7K4 ปีที่แล้ว
03 Propeller part design (Propeller Hub - Assembly)
Aircraft Propulsion - 002- Blade Element Theory
มุมมอง 10K4 ปีที่แล้ว
Aircraft Propulsion - 002- Blade Element Theory
01 Engine Mount Part's Design - Solid Edge
มุมมอง 1.9K4 ปีที่แล้ว
01 Engine Mount Part's Design - Solid Edge
Aircraft Propulsion - 001- Introduction to Propellers and Momentum Theory
มุมมอง 2.9K4 ปีที่แล้ว
Aircraft Propulsion - 001- Introduction to Propellers and Momentum Theory
Good work sir
what is the unit of the DMX
How multiply in excel sheet
sir can u pls share the pdf
Bro for when i point to workbench it 0 points what should i do
Any references for your theoretical calculations?
sir how can i model steel fiber in side concrete I am trying to use solid 65 for concrete and link 180 for the steel fiber
Do you know how to assign different materials to the two sections that were glued together? Thanks
And what is lift divergence......plz tell in comment 🙏
Sir plz tell something about lower and upper critical mach no.
A supersonic wind tunnel is designed to produce a maximum. Mach number 2 in the test section. Calculate the ratio of nozzle throat area to diffuser throat areato diffuser throat area that would allow the tunnel to function......can we write this lecture as a ans for this question
SIR UR PHONE NO?
PLZ UPLOAD MORE VEDIOS LIKE THIS,SIR DO U USE INSTAGRAM?
THANK YOU SIR
Sir can you please make a video on crack analysis on I-section and T-section.