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Vinay Goyal
เข้าร่วมเมื่อ 19 ก.ย. 2011
#calculusofvariations #aerospacestructures #structuralanalysis #finiteelements #compositematerials #abaqustutorials #vinaygoyal #nasa
This channel provides lecture series on aerospace structures, finite element methods, Abaqus tutorials, energy methods, and composite materials.
samueli.ucla.edu/people/vinay-goyal/
viterbi.usc.edu/directory/faculty/Goyal/Vinay
Biography
Dr. Vinay Goyal, is an adjunct professor at UCLA and part-time faculty at USC. He has extensive experience in the areas of launch vehicles and aircraft with emphasis in the application of advanced materials. He has over 25 years of experience, is a Technical Fellow at The Aerospace Corporation working on several launch vehicles and spacecraft. He is a member of two NASA NESC technical teams dedicated to ensure flight safety of human spaceflight. He has published over 100 technical papers in the aircraft and launch structural issues and three published books.
This channel provides lecture series on aerospace structures, finite element methods, Abaqus tutorials, energy methods, and composite materials.
samueli.ucla.edu/people/vinay-goyal/
viterbi.usc.edu/directory/faculty/Goyal/Vinay
Biography
Dr. Vinay Goyal, is an adjunct professor at UCLA and part-time faculty at USC. He has extensive experience in the areas of launch vehicles and aircraft with emphasis in the application of advanced materials. He has over 25 years of experience, is a Technical Fellow at The Aerospace Corporation working on several launch vehicles and spacecraft. He is a member of two NASA NESC technical teams dedicated to ensure flight safety of human spaceflight. He has published over 100 technical papers in the aircraft and launch structural issues and three published books.
Fireside Chat: Applications of Finite Elements to the Rapid Design of Structures with Sean Engelstad
Vinay Goyal and Sean Engelstad discussed the benefits of finite element analysis in the shortening of design cycles in the product life cycle.
มุมมอง: 749
วีดีโอ
#ABAQUS TUTORIALS: COMPOSITES MODULE 8B - Laminates versus Sandwich Structures: Buckling Performance
มุมมอง 4084 หลายเดือนก่อน
In this video tutorial we compare the buckling performance of composite sandwich structures versus laminates using #abaqus.
#ABAQUS TUTORIALS: COMPOSITES MODULE 8A - Laminates versus Sandwich Structures: Bending
มุมมอง 2624 หลายเดือนก่อน
in this tutorial we compare the bending performance of sandwich structures compared to laminates using #abaqus.
#ABAQUS TUTORIALS: COMPOSITES MODULE 7 - Design Analyses of a Aircraft Wing Using Failure Indices
มุมมอง 5254 หลายเดือนก่อน
Here we discuss several composites failure criteria that can be used to predict first ply failure. We discuss Tsai-Wu, Tsai-Hill, and maximum stress criteria. We model an airplane wing to illustrate the overall procedure on how to design a system that meet the criteria. Mr. Wei guides us through these tutorials. Failure indices are discussed in-depth here: th-cam.com/video/8d64bSw67AQ/w-d-xo.ht...
#ABAQUS TUTORIALS: COMPOSITE MODULE 6 - ABD Matrix Implementation for Composites
มุมมอง 9844 หลายเดือนก่อน
Here we learn about how the ABD matrix can be implemented in finite element software. The link below provides a deep understanding of the classical lamination theory: th-cam.com/video/CMhwNTMe_mo/w-d-xo.htmlfeature=shared The following link also provides the excel sheet and cae file used to execute the work: drive.google.com/drive/folders/1KbNFHBZp_bSrsX2VACLCrVmpnKrGmYCW?usp=drive_link
#ABAQUS TUTORIALS: COMPOSITE MODULE 4 - FREE BODY DIAGRAM PLATE ELEMENTS: SECTION FORCES & MOMENTS
มุมมอง 4864 หลายเดือนก่อน
In this video tutorial we learn how to calculate section forces and moments and how these can be queried in a finite element software. These section forces and moments are key in optimizing structures. Prerequisite to this module is the complete theory: th-cam.com/video/CMhwNTMe_mo/w-d-xo.htmlfeature=shared Files for this tutorial can be found here: drive.google.com/drive/folders/1vNvxaBr4x_Yld...
#ABAQUS TUTORIALS: COMPOSITE MODULE 5 - POST-PROCESS PLY STRESSES & STRAINS FOR 2D & 3D COMPOSITES
มุมมอง 4114 หลายเดือนก่อน
In this simple video tutorial we walk you thru how to get ply by ply stresses in a composite system using finite elements Prerequisite to this module is the complete theory: th-cam.com/video/CMhwNTMe_mo/w-d-xo.htmlfeature=shared
#ABAQUS TUTORIALS: COMPOSITE MODULE 2 - MODELING 0-deg TEST, 90-deg TEST, AND 45-deg OFF-AXIS TEST
มุมมอง 5105 หลายเดือนก่อน
In this video we simulate the simple [0]6 and [90]8 tension tests and then off axis [45/-45]2s test. These tests allow obtaining E11, E22, G12, and v12... They can also be used to find the strength in each of the directions and the shear strength as well. A link to a sample .cae file is provided drive.google.com/file/d/1SOoHKZvzGGVeTcg0zr0KG5Xf2FaZcDby/view?usp=sharing
#ABAQUS TUTORIALS: COMPOSITES MODULE 1 - MICROMECHANICS TO PREDICT PROPERTIES USING RVE
มุมมอง 1.3K5 หลายเดือนก่อน
Mr. Wei provides a tutorial on how to model an RVE to estimate composite material properties, given the fiber architecture, and fiber volume fraction. These estimates are useful in the early design process when lamina data may not be available readily. Periodic boundary conditions are used to estimate the properties. The scripts utilized to develop the models are provided here for reference: dr...
#ABAQUS TUTORIALS: COMPOSITES MODULE 3- 3D EFFECTIVE PROPERTIES TO MODEL COMPOSITES
มุมมอง 9315 หลายเดือนก่อน
Mr. Wei guides us thru the modeling of composite laminates using 3D effective properties. We also use a very useful tool in getting those properties. Files for this tutorial can be obtained here: drive.google.com/drive/folders/1Qpp8EtqH5LbpvpJNGaryjH-uXZ3lsB0y?usp=drive_link TH-cam video explaining Chou's theory to determine 3D Effective Properties th-cam.com/video/PmpXn-Ohl3s/w-d-xo.htmlfeatur...
Virtual Fireside Chat with World Renown Expert in Aerospace Failure Investigations: Mr. Thomas Brand
มุมมอง 52810 หลายเดือนก่อน
Virtual Fireside Chat with World Renown Expert in Aerospace Failure Investigations: Mr. Thomas Brand
Finite Element Analysis - Fireside Chat with Angel Lopez: Accelerating Product Development
มุมมอง 166ปีที่แล้ว
Finite Element Analysis - Fireside Chat with Angel Lopez: Accelerating Product Development
Finite Element Analysis: Fireside Chat with Chad Foerster on Personality Styles and Finite Elements
มุมมอง 204ปีที่แล้ว
Finite Element Analysis: Fireside Chat with Chad Foerster on Personality Styles and Finite Elements
Finite Element Analysis: Fireside Chat with Daniel Mueller on the Value of FEA
มุมมอง 206ปีที่แล้ว
We have invited Daniel Mueller to give a talk about the importance in the Finite Element Modeling in the design of structural systems.
22E Advanced Strength of Materials - Fatigue Fracture (Paris Law)
มุมมอง 592ปีที่แล้ว
22E Advanced Strength of Materials - Fatigue Fracture (Paris Law)
22D Advanced Strength of Materials - Fracture Prediction
มุมมอง 296ปีที่แล้ว
22D Advanced Strength of Materials - Fracture Prediction
22C Advanced Strength of Materials - Failure Prediction Examples
มุมมอง 328ปีที่แล้ว
22C Advanced Strength of Materials - Failure Prediction Examples
22B Advanced Strength of Materials - Fatigue Failure Theories
มุมมอง 310ปีที่แล้ว
22B Advanced Strength of Materials - Fatigue Failure Theories
22A Advanced Strength of Materials - Strength Failure Theories
มุมมอง 211ปีที่แล้ว
22A Advanced Strength of Materials - Strength Failure Theories
21D Advanced Strength of Materials - Castigliano's Method Applied to Beams
มุมมอง 261ปีที่แล้ว
21D Advanced Strength of Materials - Castigliano's Method Applied to Beams
21C Advanced Strength of Materials - Castigliano's Method Applied to Trusses
มุมมอง 212ปีที่แล้ว
21C Advanced Strength of Materials - Castigliano's Method Applied to Trusses
21B Advanced Strength of Materials - Castigliano's Method
มุมมอง 224ปีที่แล้ว
21B Advanced Strength of Materials - Castigliano's Method
21A Advanced Strength of Materials - Introduction to Energy Methods
มุมมอง 452ปีที่แล้ว
21A Advanced Strength of Materials - Introduction to Energy Methods
20O Advanced Strength of Materials - Composite Beam Example Problem
มุมมอง 289ปีที่แล้ว
20O Advanced Strength of Materials - Composite Beam Example Problem
20N Advanced Strength of Materials - Composite Beams Theory
มุมมอง 315ปีที่แล้ว
20N Advanced Strength of Materials - Composite Beams Theory
20M Advanced Strength of Materials - Beams with Unsymmetrical Cross Section Example Problem
มุมมอง 258ปีที่แล้ว
20M Advanced Strength of Materials - Beams with Unsymmetrical Cross Section Example Problem
20L Advanced Strength of Materials - Beams with Unsymmetric Cross Section Theory
มุมมอง 285ปีที่แล้ว
20L Advanced Strength of Materials - Beams with Unsymmetric Cross Section Theory
20K Advanced Strength of Materials - Beams with Unsymmetric Cross Section - Area Moment of Inertia
มุมมอง 164ปีที่แล้ว
20K Advanced Strength of Materials - Beams with Unsymmetric Cross Section - Area Moment of Inertia
20J Advanced Strength of Materials - Beam with Unsymmetric Cross Section - Centroid Calculation
มุมมอง 252ปีที่แล้ว
20J Advanced Strength of Materials - Beam with Unsymmetric Cross Section - Centroid Calculation
20D Advanced Strength of Materials - Beam Stress
มุมมอง 259ปีที่แล้ว
20D Advanced Strength of Materials - Beam Stress
What does node file u do?
How do you decide the amount of vent area that facesheets have if you have closed off edges. For instance, we always use corefill on the edges, but it's unclear how many holes we should poke into the facesheet to vent. I have looked for guidance on that but it's hard to find.
Hi. Where is cohesive element used here?.....Cohesive surface is defined in the interaction property
thank you so much, this video saved me for my exam, excellent explanation
this is so cool. Thank you very much
I understand the shell model would be simpler and not able to provide thro-thickness information. So what is the key difference between using model 1 and model 2?
35:30
Very good explanation, thanks!
Note to self: complete
Thanks for this simplified explanation, greetings from Iraq 🇮🇶
great are slides available?
Thank you very much
Hello, i have been trying to copy paste this NACA 2412 file by using your Python script to ABAQUS but the sketch doesnt appaer. Can you help me please? from abaqus import * from abaqusConstants import * backwardCompatibility.setValues(includeDeprecated=True, reportDeprecated=False) import sketch import part myModel = mdb.Model(name='Airfoil Project') mySketch = myModel.ConstrainedSketch(name='Base Sketch', sheetSize=2) xydata = ( (1.0000, 0.0013), (0.9500, 0.0114), (0.9000, 0.0208), (0.8000, 0.0375), (0.7000, 0.0518), (0.6000, 0.0636), (0.5000, 0.0724), (0.4000, 0.0780), (0.3000, 0.0788), (0.2500, 0.0767), (0.2000, 0.0726), (0.1500, 0.0661), (0.1000, 0.0563), (0.0750, 0.0496), (0.0500, 0.0413), (0.0250, 0.0299), (0.0125, 0.0215), (0.0000, 0.0000), (0.0125, -0.0165), (0.0250, -0.0227), (0.0500, -0.0301), (0.0750, -0.0346), (0.1000, -0.0375), (0.1500, -0.0410), (0.2000, -0.0423), (0.2500, -0.0422), (0.3000, -0.0412), (0.4000, -0.0380), (0.5000, -0.0334), (0.6000, -0.0276), (0.7000, -0.0214), (0.8000, -0.0150), (0.9000, -0.0082), (0.9500, -0.0048), (1.0000, -0.0013) ) mySketch.Spline(points=xydata)
Amazing! Thank you for such good information!
Haha love you bro
Where can I find more information about Sean's research? I would love to ask him about his critical flaw size analysis.
Thank you so much sir for sharing these informative videos
Great video. This video is very useful. Thank you.
thanks for a good lesson!
can you please tell the criteria how you select the slice thickness (or node distances) and time step?
Amazing bro😊 Give more about adhesion and composite please
These are covered they are in different playlists
THANK YOU. Once again you've saved me. Tomorrow is my final in Aerospace Structures and your playlist is what has guided me through my course. I only need a 56% on the final to maintain an A in the class and I owe it to you. Thanks for the great semester professor!
Glad I could help!
thank you very much
Thank you!!
Very instructive video, thank you.
One of the greatest tutorials ever, thank you for sharing this video , great job
how the proccess to get T1-T9 sir🙏🏻
Professor, do you have any videos covering shear centers and/or idealized structures?
I'm my book
21:14 28 MPA*, not ksi
Thank you!!
Great tutorial, quick question I have done the same procedure but I made my own model and followed your steps. but i see your origin has already been placed at 0,0,0. (Mine is somewhere else. How do I find out what the 2 origin points on my model are? currently the original has automatically been placed on the centre of the blade which is being assumed 0,0,0 and i cant generate result using that as 1st origin coordinate.)
Thank you for making these videos!
Appreciate your support
@@VinayGoyal can i ask you somthig
@@VinayGoyal please can i ask you professor
Really helpful tutorial. Thank you so much for sharing. It came out at the right time when I really needed it 🙏
Thanks for the set of lectures you have uploaded.
Hello sir in dynamic explicit can total energy become negetive ?
Yes, definitely
@@VinayGoyal in dynamic coupled temp-disp ,explicit kinatic energy compare to internal energy tends to zero .As dynamic explicit requre huge time so i want to use implicit coupled temperature-displacement/standard . Should i go for that ?
Great video about the link between Classical Laminate Theory and fem. A topic that too often is forgotten.
Hello Sir, if if one is doing the ABAQUS explicit dynamic crash analysis of composite tube (meso scale), is defining CZM for interlaminar failure necessary ?
Your video lectures are so much better than the professor I currently have! Thank you a ton!
Extremely useful video,thank you!!
useful informaation
positive zero crossings
allowable stress of fiber in helical layer and the hoop layer is the same ?
Along the fiber direction yes
Hi. Can you please provide details as to why you do not consider Sxx(x=l,y)=0? and you are using the weak form?
Is an example problem that right end is free.... There is no weak form here
Hi. can you help me. Consider a simply supported beam under uniform load transverse load on the tof the beam, why we do not put boundary conditions on Sxx (x=L, y)=0 and use the weak form?
Respected Professor thank you for uploading the video. I am working with a composite material and i need to calculate its mechanical properties but there are voids in the structure of composite you mentioned in the video that there is a method to take into account the voids present in the structure and that method is described in another video but after going through the videos i cant find that specific video can you please indicate where that video is. Thank you
Thank you sir
PLEASE REPLY TO YOUR EMAIL
Thanks you pour explanation, please, What is the reference you use for your explanations (on micromechanics)
Any composite book like Jones
Hello sir, I am currently studying civil structural engineering and would like to potentially make the transition to aerospace in the future. If I were to go for a structural position, what gaps should I fill in? Is this transtion feasible?
Very feasible is very very feasible. In fact civil engineers are very good at fundamentals which is lacking in aerospace engineers
thanks a lot for the vıdeo and the materıals.. I have been workıng on the composıtes nowadays.
Hi Vinay Sir, where can i get those two textbooks you have mentioned in the slides? also please guide about the website where you have posted the assignements.
Redshelf.com
Hello professor, what are the references used in the course?