Recent content by AIR&SPACE

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    Body-Fixed Reference Frame -- How is it useful?

    Do you mean to tell me that airplanes in Australia aren't flying upside down? LIES!
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    Troubleshooting Seldon Package Compiling Error in Visual Studio 2010

    That's the thing, though... there is no generic.h I've googled it and get two different generic.h 's : http://www.hexcodes.org/tools/netcat/Netcat/generic.h https://github.com/vlfeat/vlfeat/blob/master/vl/generic.h but there's nothing that makes me believe that either is the 'generic.h'...
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    Troubleshooting Seldon Package Compiling Error in Visual Studio 2010

    I'm having some difficulty compiling a test project within Visual Studio 2010. I'm trying to test the Seldon package, but keep getting errors during build. Specific errors I'm getting include (and vary between): // Headers from CLAPACK, downloaded at http://www.netlib.org/clapack/. //...
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    Aerospace Engineering Reading Material for a Newbie

    I've always wanted to know, what tastes better: Brontosaurus flank steak or Woolly Mammoth baby back ribs?
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    MATLAB Why is my integral function not working properly in MATLAB?

    At some point you've written a script, and called it: integral. It's probably in your root Matlab directory, or in your active directory. Matlab has a built-in function called integral, which is what the code is meant to execute. However, your version is "covering" it up. A script can't be...
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    MATLAB Why is my integral function not working properly in MATLAB?

    A month or two eh? http://www.mathworks.com/products/new_products/latest_features.html?s_tid=hp_spot_r2013a_0213
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    Molecular Modeling and Simulations

    Look into discrete element methods (DEM). That should give you an idea of how molecular modeling can be done.
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    ,CFD Simulation of Delta Wing: Questions & Guidance

    You'll probably be better off on a different forum site. Try www.cfd-online.com/Forums/
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    Aerodynamic efficiency and static longitudinal stability

    What exactly do you mean? Do you want reports dealing with either aerodynamic efficiency OR static longitudinal stability? Or a report with aerodynamic efficiency as it relates to static longitudinal stability?
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    MATLAB Gauss-Seidel iterval method using Matlab

    Well, what have you done so far? Can you make a jacobi method?
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    Does gre verbal matter for aerospace?

    My first time taking I scored: 158 (77th) Verbal 164 (90th) Quant 3.5 (30th) Writing My writing score actually got me unaccepted from several graduate schools. I had to fill out waivers to bypass admissions. So yeah, GRE scores tend to be a qualifier. A perfect score has little to...
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    How to reproduce plots from a reference paper to put in my own paper

    No problem :biggrin: I remember I downloaded the 30 day trial thinking "I'm just going to use it for the trial then get rid of it." Then I started using it and I was blown away, bought it within 10 minutes of downloading the trial, lol. It truly is an amazing program, filling an important...
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    The Mathematics of Airfoil Design

    Answer: Sort of... It depends on how you define "design" and where you're looking for the calculus. For example, a very rudimentary aspect of airfoil design, which is very limited but useful for a basic understanding of airfoil properties is Thin Airfoil Theory. Also, very important to...
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    How to reproduce plots from a reference paper to put in my own paper

    Hmmm... I guess my previous response got deleted, prob because it was a single word/link. I'll expand upon it this time. Use http://blueleafsoftware.com/Products/Dagra/, it's a free trial for 30 days, but it's worth every ($20) dollar. You import any picture file and place two lines for...
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    High School What is the error in this mathematical proof?

    The OPs friend factors out zero. For example: \frac{1*0}{1*0} would appear to be \frac{1}{1} = 1 if you factor out zero. Generally written: \frac{n*0}{n*0} \neq \frac{n}{n} That is the problem. The friend arranged the problem to \frac{0*20}{10*0} \rightarrow \frac{20}{10}...