Western Michigan University 

JAVIER M. MONTEFORT


Image of Jet Airplane Image of Jet Engine Image of Wright Brothers aircraft

ME 2560 STATICS MWR

ME 2560 STATICS TR

ME 3560 FLUID MECHANICS

Solution Test I
Solution Test II
Solution Test III
Solution Test IV
Solution Final Exam
Solution Test I
Solution Test II
Solution Test III
Solution Test IV
   
     
     
     
     


SOFTWARE

 
Calculation of Centroid
& Moment of Inertia

Truss Analysis
Frame Analysis
Shear Force and
Moment Analysis

Acknowledgements


Useful Trigonometric Formulas
Conversion Factors You May Sometime Need
Integrals. Part (a)
Integrals. Part (b)
Integrals. Part (c)

Laminar Flow Past a Circular Cylinder (Re=150) (12 MB)

Open Channel Flow (Vinlet = 2 m/s) (20 MB)