• About
    • Who We Are
    • Partners & Providers
    • News & Events
    • The ESRD Blog
    • Careers
    • Contact Us
  • Applications
    • What We Solve
    • Detailed Stress
    • Composites
    • Fracture Mechanics
    • Residual Stress
    • Sim Apps
  • Products
    • What We Develop
    • StressCheck Professional
      • StressCheck Core
      • Solvers
      • Advanced Modules
      • Utilities
      • Academic Licensing
    • StressCheck Apps
      • CAE Handbook
      • StressCheck Tool Box
    • Product Updates
  • Support
    • How We Can Help
    • Training
    • Webinars
    • Quick Start Guide
    • Help Documentation
    • Software FAQ’s
  • Simulation
    • How We Simulate
    • Benchmarks
    • Simulation Governance
    • History of FEA
    • Dictionary & Terms
  • Resources
    • Browse Our Resource Library
    • White Papers
    • Case Studies
    • Product Demos
    • StressCheck Tutorials
Serving the Numerical Simulation community since 1989
  • Contact Us
  • Register
Login
Forgot Password?
Join Us
ESRDESRD
ESRDESRD
  • About
    • Who We Are
    • Partners & Providers
    • News & Events
    • The ESRD Blog
    • Careers
    • Contact Us
  • Applications
    • What We Solve
    • Detailed Stress
    • Composites
    • Fracture Mechanics
    • Residual Stress
    • Sim Apps
  • Products
    • What We Develop
    • StressCheck Professional
      • StressCheck Core
      • Solvers
      • Advanced Modules
      • Utilities
      • Academic Licensing
    • StressCheck Apps
      • CAE Handbook
      • StressCheck Tool Box
    • Product Updates
  • Support
    • How We Can Help
    • Training
    • Webinars
    • Quick Start Guide
    • Help Documentation
    • Software FAQ’s
  • Simulation
    • How We Simulate
    • Benchmarks
    • Simulation Governance
    • History of FEA
    • Dictionary & Terms
  • Resources
    • Browse Our Resource Library
    • White Papers
    • Case Studies
    • Product Demos
    • StressCheck Tutorials

S.A.F.E.R. Numerical Simulation for Structural Analysis in the Aerospace Industry Part 1: Trends in A&D Driving Simulation

Home S.A.F.E.R. SimulationS.A.F.E.R. Numerical Simulation for Structural Analysis in the Aerospace Industry Part 1: Trends in A&D Driving Simulation

S.A.F.E.R. Numerical Simulation for Structural Analysis in the Aerospace Industry Part 1: Trends in A&D Driving Simulation

November 7, 2017 S.A.F.E.R. Simulation
SAINT LOUIS, MISSOURI – November 7, 2017

Relentless Business Drivers in the Aerospace & Defense Industry

The global aviation, aerospace, and defense industries face unrelenting pressure for ever-increasing levels of operational performance, lifecycle reliability, and mission robustness in their products, platforms, and programs delivered to commercial and military customers. This is occurring concurrently with greater demand for overall system performance that is faster, lighter, quieter, smarter, greener, and more connected. And of course, customers want all of this and more at less cost to procure, reduced time to deploy, and cheaper to maintain!

These business drivers have unleashed a level of interconnected complexity across nearly every organizational function, R&D process, and product line of the modern A&D enterprise. A new norm of debilitating complexity permeates today’s aerospace business throughout program management, requirements planning, system design, engineering analysis, manufacturing workflows, product line variants, supply chain collaboration, and in-service sustainment. While dozens of promising new technologies, software tools and enterprise solutions have emerged in recent years to advance these organizational functions, they have unfortunately added yet more layers of technical complexity along nearly every axis.

The U.S. Navy’s aircraft fleet requires high-fidelity structural analysis for design and to keep airborne over a longer lifecycle

A&D Program Pains and Engineering Stresses

While many OEM prime contractors and their supply chain partners have risen to meet the challenge of greater performance and higher complexity, others have struggled as evidenced by the number of major programs which encounter substantial overruns in budget or schedule, or both. Not that long ago the U.S. GAO reported that major defense programs experienced an average schedule delay approaching two years, with an average budget overrun of more than 25%.

As this trend is unsustainable, program managers are under substantial pressure to revisit obsolete assumptions and defend legacy thinking that impacts the technology maturity curve. One such example is the expectation that years of investment in the automation, standardization, and integration of tools for CAD, CAE, CAM, PDM, Visualization, and DMfg now make high concurrency of final design, tooling, testing, and manufacture of production aircraft less risky.

The inconvenient truth is that simultaneous advancements across numerous technology silos often injected more complexity and time than expected, and in doing so created new systemic risks especially after they were connected and integrated. As a consequence, there was often less, not more, time left in the schedule for final prototyping, optimization, supply chain collaboration, and flight testing. The pains of a new program often became the new stresses on engineering.

The high performance of the Boeing 787 Dreamliner is made possible by a complex interdependent global network of partners and suppliers with design engineering contributions, not just manufacturing.

Diminishing Returns from Investing in More of the Same Technology

Faced with an avalanche of complexity, many legacy technologies – along with the organizational competencies, workflows, and tools built upon them – have become non-linear to further investments for improving. That is, an incremental improvement in one function does not always translate into immediate or scalable improvements across the entire product development ecosystem. Some highly-touted advancements often introduce more uncertainty and complexity than the interdependent web of new product development can quickly absorb. Aerospace managers have come to realize that a seductive innovation in one domain may cascade into a series of downstream hurdles that are not always fully understood at the onset of the new technology adoption maturity curve.

In response to schedule-eating, budget-busting complexity, engineering groups are seeking new methods and tools that aren’t limited to more of the same advancements to their organization’s competency and capacity to meet higher product performance requirements. They now demand that new investments also begin to distill out complexity and wring out risk which has become increasingly tricky to define and unwieldy to manage. Particularly attractive are new methodologies and technologies that are conceptually so simple, reliable, and robust that they may be used with confidence by engineering specialists as well as non-experts alike.

Simulation technologies and analysis software used in the structures, stress, strength, DaDT, materials, and manufacturing support groups are particularly ripe for simplification and “robustification”. Only then can the promise of the democratization of simulation to compress product development cycles through simulation-driven design finally be achieved, without adding yet more complexity and risk.

The State of Simulation and Modeling in Aerospace Engineering Groups

Over a period of four decades, application software developed for performing simulation based on the finite element method (FEM) has matured to deliver an ever-expanding list of functionality and features across a steadily widening computational spectrum of multiple physics. As finite element analysis (FEA) software products became more capable and feature-rich, they also became more complex to learn, time consuming to master, prickly to operate, and problematic to trust. FEA is justifiably referred to as an “art form” for expert analysts due to all the sources of assumptions, approximations, idealizations, discretizations, judgements, and errors an engineer must deal with to arrive at a “good” solution which they can defend in a design review.

What element type(s) and size(s) are best for performing detail stress analysis using legacy FEA codes – only the experts know!

The evidence speaks for itself that when different users attempt to solve the same computational mechanics problem by using different FEA software – or employing the same code but with subjectively different models, meshes, and element types used – it is not unusual to generate very different analytical results. It is no secret to the experts and their managers that most of the effort and time of FEA is spent in the laborious pre-processing steps of creating bad models to finally arrive at good ones, instead of in the post-processing stage leveraging the results to optimize design performance. Simulation analysts with deep FEA expertise rightfully take pride in their profession for mastering all the nuances and minutia which can influence the quality of their work.

As a consequence, some aerospace engineering managers think of FEA as definitely the best analysis tool for the highest quality results, but only after all other analysis methods have been exhausted! The use of engineering handbooks, design curves, empirical data, closed form solutions, previous designs, and elaborate spreadsheets to calculate and pencil-whip margins of safety is seen as preferable to spending more time building, running, debugging, and tuning finite element models. This is not to discount the power and accuracy of finite element-based stress analysis – especially when compared to the alternative of more physical testing – but just an honest assessment that there is a very significant cost to obtain the higher-fidelity solutions that FEA offers.

Engineering handbooks like he MIL-HDBK-5H and Roark’s Formulas for Stress and Stress are frequently extended well outside of their ranges, resulting in more errors and unknowns

Coming Up Next…

In Part 2 of this S.A.F.E.R. Simulation series we will examine the increasing demands on the structures engineering simulation function and the often misunderstood challenges they experience when using legacy analysis technologies based on the finite element method. The origins and differences between finite element modeling and predictive computational numerical simulation will be summarized. The capabilities of ESRD’s numerical simulation technology base, and software products build upon it including StressCheck™ and Smart Sim Apps in a Digital CAE Handbook, will be overviewed. In Part 3 we will profile use-case examples from A&D that substantiate the benefits to engineers and value to their programs from the use of a newer generation of smarter simulation software that is Simple, Accurate, Fast, Efficient, and Reliable – S.A.F.E.R – for both the frequent expert and occasional non-expert user alike.

To receive future S.A.F.E.R. Simulation posts…

=
Loading
Tags: Aerospace and DefenseDetailed StressFatigueNAFEMSSimulation Governance
2

You also might be interested in

‘How Do You Verify the Accuracy of Engineering Simulations?’ Webinar Recording Now Available
Convergence of minimum principal stress in an aircraft keel beam structure (courtesy Digital Engineering).

‘How Do You Verify the Accuracy of Engineering Simulations?’ Webinar Recording Now Available

Jan 16, 2019

On Wednesday, January 16, 2019 a webinar titled “How Do You Verify the Accuracy of Engineering Simulations?” was provided by ESRD’s Gordon Lehman and Brent Lancaster. In case you missed it, the webinar recording is now available!

S.A.F.E.R. Numerical Simulation for Structural Analysis in the Aerospace Industry Part 5: An Introduction to StressCheck for High-Fidelity Aero-structure Analysis
C130 Hercules transport aircraft.

S.A.F.E.R. Numerical Simulation for Structural Analysis in the Aerospace Industry Part 5: An Introduction to StressCheck for High-Fidelity Aero-structure Analysis

Apr 2, 2018

In this final post of our "S.A.F.E.R. Numerical Simulation for Structural Analysis in the Aerospace Industry" series, we will profile the stress analysis software product StressCheck®, what makes it different from other FEA software and the applications for which it is used in A&D engineering.[...]

Digital Twins

Digital Twins

May 2, 2024

The idea of a digital twin originated at NASA in the 1960s as a “living model” of the Apollo program. When Apollo 13 experienced an oxygen tank explosion, NASA utilized multiple simulators and extended a physical model of the spacecraft to include digital simulations, creating a digital twin. This twin was used to analyze the events leading up to the accident and investigate ideas for a solution. The term "digital twin" was coined by NASA engineer John Vickers much later. While the term is commonly associated with modeling physical objects, it is also employed to represent organizational processes. Here, we consider digital twins of physical entities only.

Leave a Reply

We appreciate your feedback!
Cancel Reply

You must be logged in to post a comment.

Looking for Resources?

Interested in a Demo, Evaluation or Purchase?

Have a Software Question, Issue or Feature Request?

Recent News & Events

  • Trustworthiness in Simulation: Credibility or Decision-grade Reliability?
  • Beyond the Black Box: Explainable AI Requires Explainable Simulation
  • Turtle Shells and Legacy Finite Element Codes: Evolutionary Constraints in the Age of Explainable AI

Quick Links

  • Quick Start Guide
  • Documentation
  • Software FAQs
  • Software Demos

Testimonials

  • “As the United States Air Force continues to extend the service life of their aircraft the Aircraft Structural Integrity Program (ASIP) has had to refine the methods it uses to analyze and predict fatigue crack growth. Through the use StressCheck, coupled with AFGROW, we in A-10 ASIP have been able to more accurately model, predict and analyze critical aircraft structure for the A-10 and other types of structure for non-A-10 system managers. This also allows us within the A-10 to more accurately assess risk for decision makers, streamline aircraft inductions into scheduled maintenance and reduce cost for total life cycle management.”

    A-10 ASIP Manager

Testimonials

“As frequent StressCheck users we rely on the capabilities and reliability of the program to complete our everyday jobs ensuring safe reliable flights of our aircraft. The layout of the program and documentation allow for a quick learning process and the support ESRD offers is second to none. They take the time to answer the most basic questions as well as working through complex problems to ensure the proper validation of results. The effort they make in satisfying their users needs increase the reliability, functionality, and capability of this great program.”

USAF Engineer, Hill Air Force Base

Member Portal

  • Member Registration
  • Member Login

Contact Us

© 2026 · Engineering Software Research & Development, Inc. | Terms & Conditions | Privacy & Cookie Policy | Software License Agreement | Software Maintenance and Technical Support Policy

Prev Next

We use cookies on our website to give you the most relevant experience by remembering your preferences and repeat visits, as outlined in our Cookie Policy. You may adjust your cookie preferences within .

ESRD
Powered by  GDPR Cookie Compliance
Privacy Overview

This website uses cookies to improve your experience while you navigate through the website. Out of these, the cookies that are categorized as necessary are stored on your browser as they are essential for the working of basic functionalities of the website. We also use third-party cookies that help us analyze and understand how you use this website. These cookies will be stored in your browser only with your consent. You also have the option to opt-out of these cookies. But opting out of some of these cookies may affect your browsing experience.

Strictly Necessary Cookies

Strictly Necessary Cookies should be enabled at all times so that we can save your preferences for cookie settings.