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B.J. Jasinski wrote: > > hi all, > > i'm doing a project for a class which involves a lap-time simulation of > an indycar. i have been researching the parameters (i.e. geometry, > mass, moment of inertia) of the whole car and various parts of the car > that i need, and i would like to get some verification if anyone knows > more than i do. > > here's the parameters i am having trouble determining: > > Chassis: > -------- > mass=715kg (i have also found other values up to 905 kg, i'll > probably use an average of the 2) > Izz=1525 kgm^2 (by approximating the chassis as a rod, and > wheels as point masses, i calculated 775 kgm^2. > which is closer? i got the 1525 kgm^2 from SAE > paper 910012, but i'm not sure i believe it) > Af=1.0 m^2 (frontal area - i estimated this from car > drag mesasurements) > > Engine: > ------- > Power=850hp (634kW) > Max RPM = 13800 (1445 rad/sec) > > These values give an engine torque at max rpm of 438Nm, is this > realistic? > > Final Drive Ratio= 4.09 (got this from SAE paper 910011 for a 5th gear, > is this also realistic?? estimating some > values i calculated 3.25) > > Wheels: > ------- > radius = 0.33m > Iyy = 0.89kgm^2 to 1.29kgm^2 (i will most likely average these values > for the final simulation.) > > just in case it matters, the project is due on friday, and i would > appreciate a quick response. > > thanks in advance, > b.j. > > -- > B.J. Jasinski > In the past, we've given folks a bad time for expecting the newsgroup to do their homework for them. In this case, it looks like B.J. mostly needs a reality check on the numbers. I can't help with that, but surely we've got someone that can. Come on folks, it's close to Christmas.....8^) -- Alan K. Gideon, P.E. | Naval Architect & Marine Engineer | akgideon@mindspring.com "If you're not still learning, you've already retired - your boss just hasn't noticed yet." Peter Coffee, November 1996Return to Top
Can you help out? Have a look at our web page at www.alloytech.comReturn to Top
In sci.engr.mech Enrique JuaristiReturn to Topwrote: [ANSYS newsgroup proposed] : If you agree with this, please reply to this message on the newsgroups. I : am not familiar with the workings of the Newsgroups, but if we are enough : interested people we might create something worth the while! 6 of us here use ANSYS everyday and would be very interested in an ANSYS newsgroup!! Leslie (and Jim, Wei, Nader, Bill, Doug) LORD Corporation -- ___________________________________________ Leslie P. Fowler lfowler@acm.vt.edu leslie_fowler@lord.com http://acm.vt.edu/~lfowler ___________________________________________
John Ciprian Applied Science Teacher Greene County Career Center 2960 W. Enon Road Xenia, OH 45385 (513) 426-6636 gccc_jcipria@k12server.mveca.ohio.gov I am looking for Young's modulus for balsa wood to design bridge trusses--would appreciate your help very much. Thank you.Return to Top
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When applying loads to axisymmetric elements in COSMOS (PLANE2D), are the loads specified in units of force (lb) or in force/length (lb/in)? The documentation doesn't say, and I don't have a lot of condidence in SRAC's tech support (the person I talked to said force/length, but he didn't sound very confident). The reaction forces sum to the total nodal loading, but the output file still doesn't specify units. Thanks in advance. -- Barry Berenberg Los Alamos National Laboratory ESA-DE berenberg@lanl.govReturn to Top
gccc_jcipria@k12server.mveca.ohio.gov wrote: > > John Ciprian > Applied Science Teacher > Greene County Career Center > 2960 W. Enon Road > Xenia, OH 45385 > (513) 426-6636 > gccc_jcipria@k12server.mveca.ohio.gov > > I am looking for Young's modulus for balsa wood to design bridge trusses--would > appreciate your help very much. > > Thank you. A glossy wall chart (Ashby, 1994) in my office has balsa sitting at somewhere between 4-7GPa. I don't have anything more detailed. Hope that helps IanReturn to Top
I am working on this topic for my thesis along with its modeling. any usefull idea is wellcomed. ThanksReturn to Top
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SYALE (SYALE@prodigy.net) wrote: : Does anyone have the names of some fabricators in Germany who can build : welded aluminum silos to store plastic pellets. Would appreciate any : help. : Steve Yale I think there is Aluminium Rheinfelden - VACONO. They deal with tank structures made of aluminium and some other stuff. If I remember well, their web-page is on http://www.vacono.com . Bye, Ben -- ------------------------------------------------------------------- Benedikt Schauder INSA de Lyon / LBS - Bat. 304 | tel :(33)-72-43-58-15 F-69621 Villeurbanne cedex | fax :(33)-72-43-85-23 ------------------------------------------------------------------- e-mail: schauder@gcu-beton.insa-lyon.fr -------------------------------------------------------------------Return to Top
Hi ! I am studying mechanical engineering in Germany. Part of mystudies is a five - month practical term at a company in order to use the gained theo- retical knowledge in pratical work. Therefore I am searching for american companies, dealing with construction of mechanical engines and equipments in order to poste them my application. You would be a great help if you could name me a few american companies ( I will look for their addresses for myself ), preferably major companies. Please send me a private mail ! Thank you very much Bye, Frank BongartzReturn to Top
hobdbcgv@aol.com (Hobdbcgv) wrote: > I love the Limbaugh approach to problems.< funny, I don't really think of Limbaugh as "leftist"Return to Top
In articleReturn to Top, berenberg@caent3.esa.lanl.gov () wrote: >When applying loads to axisymmetric elements in COSMOS (PLANE2D), are >the loads specified in units of force (lb) or in force/length (lb/in) Applied forces and computed reactions are in units of pounds per radian--total load/2pi. So the axial loading on a cylindrical shell under internal pressure is (pressure*pi*radius^2)/(2*pi) = pressure*radius^2/2. Pressures are input in psi. You might want to get comfortable with all this by running a simple model of a plate or spherical shell and going over the input file carefully. I'm not surprised you had trouble with SRAC technical support on a simple (for them) question like this. I got a buckling eigenvalue of exactly unity once, and the phone voice told me I'd just gotten lucky with my choice of loads. In fact the buckling solver was breaking down because I'd used constraint relationships in the problem. Christopher Wright P.E. |"They couldn't hit an elephant from chrisw@skypoint.com | this distance" (last words of Gen. ___________________________| John Sedgwick, Spotsylvania 1864) http://www.skypoint.com/subscribers/chrisw
The TrueGrid WEB page has been moved. It is now located at http://truegrid.com Robert Rainsberger XYZ Scientific Applications, Inc.Return to Top
> > >If you are are a user of either Ansys or MSC, I would greatly appreciate > >some feedback (positive or negative). You have to realize that the age-old battle - ANSYS vrs NASTRAN is like trying to get the Orange Irish to make peace with the Green Irish. Amoung FEA users the cultural differences and loyalties run very deep (beyond reason many times). Maybe it has to do with which code you learn first. but here's my 2 cents worth -- I've used both (ver 5.2 ANSYS and Ver 68 MSC/NASTRAN as well as CSA/NASTRAN) and I have to say that both ANSYS and NASTRAN are good solid products. It kind of depends on the types of problems you are solving. ANSYS's parametic input stuff is nice and NASTRAN's DMAP is nice too. Since I have been doing mostly static stress and dynamics analyses (modes, sine, random) I have to say that NASTRAN (both MSC and CSA versions) beat ANSYS hands down for ease of using in this area. The DAMP feature is very powerful. Try doing a cross-orthogonality check of FEA [phi] against modal test data. ANSYS - it will be a bit difficult - with a DMAP alter in NASTRAN (MSC, CSA or UAI) it is a snap. I have felt that MSC and CSA user support was better than ANSYS support. one time, I called the Swanson Penn. office and the guy on the hotline was *very* short with me because I was calling him instead of their California office (it was 6 AM, the CA office was not open). MSC never has done that to me. - Tom Wolverton, P.E.Return to Top
A-REFReturn to Topwrote: >> > >What is a Stationary engineer? It's not a term I've come across in the >UK civils industry. Save, perhaps, to describe an engineer >having a nap in a slow afternoon :) > >-- >Shaun Lewis, The Dredging and >Assistant Estimator Construction Company Ltd. I believe a stationary engineer is one who operates and maintains power plants (i.e. steam power plant for heating buildings). You can often find them in boiler rooms in large buildings or industrial plants. Sometimes, they are also called "power engineers" although the subtle distinction between the two is not clear. T.Kwok
Not sure if my earlier post made it here... I got cut off as I was sending. Anyway, there is a table of Indycar data on pp 825 of our book, "Race Car Vehicle Dynamics". It has some of what you want. Not sure why you need yaw inertia for a lap time simulation -- good, smooth drivers _minimize_ yaw acceleration, to save the lateral tire forces for actual lateral acceleration... Anyway, the pitch inertia in the table will be nearly the same as the yaw inertia. Car weights vary by several hundred pounds, depending on fuel loading. Available engine power changes every year with rules changes, I'm not up on this. Air drag and downforce change with every track that they run on, as do all the gear ratios. A good simple use for a lap time simulation (given reasonable engine and aero data) is to _choose_ the gear ratios... Sincerely, -- Doug Douglas MillikenReturn to TopMilliken Research Associates Inc. -------------------------- On Wed, 18 Dec 1996, B.J. Jasinski wrote: > hi all, > > i'm doing a project for a class which involves a lap-time simulation of > an indycar. i have been researching the parameters (i.e. geometry, > mass, moment of inertia) of the whole car and various parts of the car > that i need, and i would like to get some verification if anyone knows > more than i do. > > here's the parameters i am having trouble determining: > > Chassis: > -------- > mass=715kg (i have also found other values up to 905 kg, i'll > probably use an average of the 2) > Izz=1525 kgm^2 (by approximating the chassis as a rod, and > wheels as point masses, i calculated 775 kgm^2. > which is closer? i got the 1525 kgm^2 from SAE > paper 910012, but i'm not sure i believe it) > Af=1.0 m^2 (frontal area - i estimated this from car > drag mesasurements) > > Engine: > ------- > Power=850hp (634kW) > Max RPM = 13800 (1445 rad/sec) > > These values give an engine torque at max rpm of 438Nm, is this > realistic? > > Final Drive Ratio= 4.09 (got this from SAE paper 910011 for a 5th gear, > is this also realistic?? estimating some > values i calculated 3.25) > > Wheels: > ------- > radius = 0.33m > Iyy = 0.89kgm^2 to 1.29kgm^2 (i will most likely average these values > for the final simulation.) > > just in case it matters, the project is due on friday, and i would > appreciate a quick response. > > thanks in advance, > b.j. > > -- > B.J. Jasinski > > Graduate Research Assistant > Department of Aeronautical & Astronautical Engineering > University of Illinois at Urbana Champaign > (217) 244-0492 fax: (217) 244-0720 > e-mail: wjasinsk@uiuc.edu > http://www.students.uiuc.edu/~wjasinsk/ > > "Without love in a dream, it will never come true..." > >
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I would appreciate any leads on this question. We are trying to replace the stud bolts in a studding outlet. The bolts in a similar connection (6" 1500#) were M36x4. The only metric sizes near this appear to be M35x1.5 and M36x2. I'm afraid the bolt we removed is either a M35x3 (which I can find no published information supporting this) or a stretched 1 3/8-8 UN. I am in desperate need of answering this question quickly. Thanks, Jeff Lester, P.E. Phoenix Exchanger WorksReturn to Top
Marc wrote: > > hi, > > need supply of polypropelene instr. connection heads 1/2 x 3/4 made by > a > company in the USA. Looking for the manufacturer. I have been dealing > > with a distributor but getting bad service. Want to buy from the > manufacturer in reasonable quantity (hundreds at a time) but cant find > > who makes them. Any help ? you might try: http://www.thomasregister.com:8000/Return to Top
Tashko Sarakinov - MECE/W94 wrote: > > Greetings folks. I'm trying to track down the propeties of > aluminum alloy 7005. All of the materials books I have looked > into do not mention it. Is it relativly(sp?) new? > I actually need it for my thesis of a bicycle that is constructed > from 7005. I'm not sure what treatment the frame has but if > somebody has any information at all I would appreciate it. > > Regards, > > Tashko. Hello there, I am not aware of any Aluminum Alloy 7005 but I do know that Reynolds manufactures a 7050 and 7001 Aluminum alloy (UNS # A97050 and A97001 respectively). The 7050 is an aircraft sturcture alloy that is available in bar and tube stock. The 7001 is also a high strength structural alloy that comes in bar and tube. Hope this helps. AlasdairReturn to Top