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						<h1>Analysis</h1>
						<p>
							CDI-Aerospace offers complete analytical engineering solutions to the aerospace industry. 
							Our capabilities include linear and non-linear finite element analysis, dynamics and 
							component modal synthesis, kinematics, fatigue, damage tolerance, and crack growth analysis, 
							as well as basic classical aircraft stress analysis.  
						</p>
						<p>
							We also provide full structural test support, from simple specimen testing to develop 
							material allowables, to full-scale ultimate testing of large structural assemblies.  
							As a part of the structural substantiation effort we also, as required, support findings 
							of compliance with the pertinent airworthiness authority requirements (FAA, JAA, CAA, etc.).  
							CDI-Aerospace works directly with the client to engineer analysis solutions that work 
							precisely to the project's defined goals and specifications.
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						<p>
						  Our capabilities also include integrated full-engine analysis. We can analyze full-engine 
						  solid models as well as structural, thermal, gas flow-path, and secondary flow-path 
						  models in support of complex turbomachinery designs. These complex finite-element models include 
						  rotating and static systems to allow refined analysis of the following: 
						</p>
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							<ul>
								<li>Engine flight envelope blade and seal clearances</li>
								<li>Rotor thrust calculations</li>
								<li>Preliminary stress, bolted joint and models</li>
								<li>Asymmetric loading and response</li>
								<li>Boundary conditions for systems or component studies</li>
								<li>Dynamic loads analysis (FBO, Bird Strike)</li>
							</ul>
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						<p>
							Our analysis team uses the latest software tools and technical knowledge to properly 
							identify and evaluate all the possible environments and risks that could impact the 
							component throughout its lifetime of operation.   We specialize in commercial, military, 
							and private aircraft primary structures, composites, interiors, landing gear, and systems, 
							as well as engines, nacelles, struts, and all related secondary structural components.
						</p>
						<p>
							We offer flexibility in software solutions by providing custom GUIs and menu driven 
							parametric design and analysis tools and utilities, with complete software integration, 
							including development with Patran, Nastran, Ansys, Femap, and others.  This includes 
							customized programming in VB, Perl, Fortran, PCL, and APDL.
						</p>
						<p>
							CDI-Aerospace also provides the option of customizing Patran, Nastran, and Ansys using 
							customer specific requirements and/or our own vast libraries of advanced scripts, functions, 
							and macros.  CDI-Aerospace also has multiple geometry transfer services available utilizing 
							a variety of geometry engines and file formats.
						</p>
						<h3>Our Capabilities</h3>
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							<ul>
								<li>Classical Airframe Structural Analysis</li>
								<li>Finite Element Analysis - Steady State and Transient</li>
								<li>Heat Transfer and Thermal Analysis</li>
								<li>Advanced Analysis - Non-Linear Material, Contact, Geometric</li>
								<li>Dynamic Analysis - Modal, Frequency Response, Vibration, PSD, Full Transient (Explicit)</li>
								<li>Composites Analysis</li>
							</ul>
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							<ul>
								<li>Life Analysis (Fatigue, Crack Growth, and Damage Tolerance)</li>
								<li>Computational Fluid Dynamics</li>
								<li>Gearbox Analysis</li>
								<li>Tolerance Analysis</li>
								<li>Mass Properties Analysis</li>
							</ul>
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						<h3>Turbomachinery Capabilities</h3>
						<ul>
							<li>
								<h4>Finite Element Analysis</h4>
								<ul>
									<li>Static structures, dynamic analysis and rotating components</li>
									<li>Coupled structural/thermal</li>
									<li>Heat transfer</li>
								</ul>
							</li>
							<li>
								<h4>Combustion Analysis</h4>
								<ul>
									<li>Aerothermal design of combustion systems </li>
									<li>Diffuser design and development</li>
									<li>Research and evaluation of burners, ignition units and heater controls</li>
								</ul>
							</li>
							<li>
								<h4>Aerodynamic Analysis </h4>
								<ul>
									<li>Aerodynamic design / development </li>
									<li>1, 2 and 3D CFD modeling </li>
									<li>Aerodynamic testing </li>
									<li>Analysis of flight test data </li>
								</ul>
							</li>
							<li>
								<h4>Performance Analysis</h4>
								<ul>
									<li>Preliminary design support </li>
									<li>Data reduction </li>
									<li>Cycle modeling </li>
									<li>Development and calibration of engine test facilities </li>
									<li>Engine Performance Analysis</li>
								</ul>
							</li>
						</ul>
						<h3>Airframe Structure Capabilities</h3>
						<ul>
							<li>
								<h4>Finite Element Analysis</h4>
								<ul>
									<li>Linear: Static, Buckling, Composites</li>
									<li>Non-Linear: Material, Contact, Geometric, Buckling, Transient</li>
									<li>Dynamic: Linear &amp; Non-Linear, Explicit, Modal, Frequency Response, Vibration, PSD, Full Transient</li>
									<li>Direct CAD Access For Meshing</li>
									<li>2D/2.5D/3D Modeling</li>
									<li>Fatigue and Fracture Mechanics</li>
								</ul>
							</li>
							<li>
								<h4>Durability and Damage Tolerance</h4>
								<ul>
									<li>Load spectrum and reconstructed stress history</li>
									<li>Cycle-Counting</li>
									<li>Critical components selection (PSE)</li>
									<li>Stress intensity factors and ß Model</li>
									<li>Crack growth analysis</li>
									<li>Retardation</li>
									<li>Residual strength analysis</li>
									<li>Inspection intervals and methods</li>
									<li>Documentation and certification reports</li>
									<li>Repairs (fleet support and discrepancies)</li>
									<li>Test support</li>
								</ul>
							</li>
						</ul>
						<h3>Software Competencies</h3>
						<div class="ListColumn">
							<ul>
								<li>NASTRAN</li>
								<li>PATRAN</li>
								<li>ANSYS</li>
								<li>ANSYS WORKBENCH</li>
								<li>MATLAB / SIMULINK</li>
								<li>ABAQUS</li>
								<li>FEMAP</li>
							</ul>
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								<li>COSMOS</li>
								<li>COSMOSWORKS</li>
								<li>CRACKS 98</li>
								<li>NASA / FLAGRO</li>
								<li>FLUENT</li>
								<li>DYTRAN</li>
								<li>LS/DYNA</li>
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