Applied Mechanics Division
HH-60G Finite Element Model and DTA
HH-60G Loads / Environment Spectra Survey
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Applied Mechanics
Mechanical Design
Information Systems
Reliability and Human Engineering
Electronic Systems
Embedded Systems
Logistics Services
Engine Truss Mount Analysis
© 1987-2012 Mercer Engineering Research Center 135 Osigian Blvd. • Warner Robins, GA 31088
info@merc-mercer.org • www.merc-mercer.org • 478.953.6800
Mercer Engineering Research Center (MERC) has performed structural analyses of the C-130J Under Wing countermeasures dispensing system (CMDS) and aircraft backup structure to assess the structural impact of dispensing improved countermeasures. MERC utilized dynamic analyses of single shot and multiple shot (salvo) configurations using measured recoil loads to evaluate the safety margins of critical components and the effect of dispense interval on the fatigue life of the structure.
Sample project below - select a project link to view additional information
C-130 Truss Mount Lug Structural Analysis
Condition Based Maintenance
Fire Control Computer Electronics Thermal Modeling
AC-130H Corrosion Effects Analysis
Flare Launch Analysis
NDI Procedure Development
Targeting Pod Circuit Card Shock Loading Evaluation
Helicopter Tailboom Misalignment Effects on Fatigue
Tow Tractor Testing and Analysis
School Bus Safety Study
Aircraft Damage Tolerance Analysis
UH-1N Flight Data Acquisition
Featured Projects
•Thermal Analysis
•Structural Dynamics
•Static Stress Analysis
•Shock / Vibration Analysis
•Linear and Non-Linear Mechanics
•Impact/Crash Analysis
•Fracture/Fatigue/Crack Growth Analysis
•Flight and Ground Vehicle Data Acquisition
•Finite Element Analysis
•Automated Maintenance Data Collection
•Aircraft Structural Integrity Program (ASIP) Support
Areas of Expertise
The Applied Mechanics Division (AMD) offers a broad range of analytical capabilities that provide timely, cost-effective, practical solutions to our customers’ needs. The staff has extensive test and analysis experience; credentials include undergraduate and graduate engineering degrees up to and including the doctorate level. Finite element modeling capabilities include meshing/preprocessing with tools such as FEMAP and HyperMesh, and importing geometry from a variety of CAD and solid modeling platforms like SolidWorks, Catia, and AutoCAD. Linear and non-linear solutions to static and dynamic problems are found using NASTRAN and LS/DYNA solvers. When special post-processing capabilities are required, the MERC staff is highly proficient at creating unique applications with advanced engineering tools like MATLAB, PERL, and FORTRAN. AMD provides durability and damage tolerance analysis, and is proficient with spectra generation codes and with crack growth codes like FRANC2D, FRANC3D, and AFGROW. The division supports Aircraft Structural Integrity Programs and related tasks for a range of USAF platforms including C-130, C-5, F-15, UH-1N, and HH-60G aircraft. These tasks include maintenance data collection and analysis, NDI procedures, Force Structural Maintenance Plans, ASIP master plans and Loads/Environment Spectra Survey development.
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