CRashworthiness for Aerospace Structures and Hybrids · UB MAE

The
CRASH Lab

We model, test, and design aerospace systems for impact, collision, and extreme environments — studying what happens when structures meet their limits.

Explore research

Domain 01 · Collision Dynamics

Crashworthiness
& Impact Dynamics

High-speed impact, hypervelocity events, and penetration mechanics. We quantify how aerospace materials absorb, deflect, and fail under dynamic loading — and redesign from those first principles.

Space Systems · Bioinspired Design

BREEZE:
Venus Atmospheric Explorer

A NASA NIAC–funded spacecraft inspired by the pectoral-fin motion of a manta ray, designed to soar on the 370 km/h winds of Venus's upper atmosphere — where surface conditions are too extreme for conventional landers.

Concept representation — CRASH Lab / NASA NIAC program

Mission

Engineering survival
at the edge of impact.

  • 150+ UAS models simulated
  • 06 Active research domains
  • NIAC NASA-funded mission concept
  • UB · MAE Dept. of Mechanical & Aerospace Eng.

The CRASH Lab — CRashworthiness for Aerospace Structures and Hybrids — is a research group within the Department of Mechanical and Aerospace Engineering at the University at Buffalo, led by Dr. Javid Bayandor.

We use sophisticated computational simulations and experimental analysis to model real-world collision events, stress failure modes, and the structural response of aerospace systems in extreme environments. Our work directly informs the design of safer aircraft, smarter unmanned systems, and more resilient spacecraft.

Research

Domains

02

Crashworthiness & Ballistics

High-speed impact, hypervelocity events, and penetration mechanics. Structural analysis of how aerospace materials absorb, deflect, and fail under rapid dynamic loading.

03

Advanced Aerospace Structures

Hybrid composite structures, multi-material systems, and airframe architectures designed for maximum energy absorption and structural survivability in impact scenarios.

04

Space Exploration & Mission Design

Re-entry vehicles, planetary landers, and sample-return capsules — from Venus atmospheric entry dynamics to Mars surface impact modeling.

05

Bioinspired Flight & Robotics

Vehicles and robotic systems derived from biological models: stingray-wing spacecraft concepts, biomimetic aerodynamic structures, and adaptive flight mechanisms.

06

Fluid–Structure Interaction

Computational FSI modeling of aerodynamic loading, flow-driven structural deformation, and fluid coupling in aerospace and high-speed impact scenarios.

Methods

How we work

  1. Model

    Computational Simulation

    Finite element modeling, CFD, fluid–structure interaction, and high-fidelity impact simulation to replicate real-world collision events at operational scale.

  2. Simulate

    Structural Dynamics Analysis

    Dynamic loading, modal analysis, energy absorption modeling, and failure-mode prediction across advanced aerospace material systems.

  3. Validate

    Impact & Ballistics Testing

    Experimental validation of simulation models through controlled impact testing, high-speed imaging, and instrumented structural response measurement.

  4. Redesign

    Aerospace Design & Optimization

    Mission-driven design of aerospace systems — from structural topology to mission architecture — optimized for survivability and performance in extreme environments.

Projects

Active & ongoing work

Collision · Safety

UAS–Aircraft Strike Database

A library of 150+ UAS models simulated at flight-realistic speeds and geometries against full-scale aircraft structures — quantifying structural damage to inform aviation safety standards.

Impact · Structures

Hypervelocity & Ballistics Research

High-speed penetration mechanics and structural survivability modeling for aerospace and defense applications under hypervelocity impact conditions.

Space · Landing

Planetary Entry & Landing Systems

Re-entry dynamics, descent control, and surface impact modeling for planetary probes, sample-return capsules, and Earth entry vehicles — from structural concept to mission architecture.

People

The lab

Dr. Javid Bayandor

Principal Investigator · Associate Professor, MAE · University at Buffalo

Dr. Bayandor leads the CRASH Lab's research across crashworthiness, advanced aerospace structures, bioinspired systems, and space mission design. His work spans computational simulation, experimental impact analysis, and aerospace vehicle development for civil, defense, and space applications.

PhD Researcher

Crashworthiness & Simulation

PhD Researcher

Space Structures & Entry

MS Researcher

Impact Dynamics

Undergrad Researcher

Bioinspired Systems

Join the Lab

PhD Research MS Research Undergrad Research

The CRASH Lab recruits graduate researchers and undergraduate team members interested in aerospace impact dynamics, computational simulation, spacecraft design, and high-consequence structural engineering. Prospective PhD and MS students are encouraged to reach out directly.

Reach out →

Collaborate

Work with the CRASH Lab

We partner with aerospace industry, government agencies, space research institutions, and academic collaborators on crashworthiness, simulation, and aerospace systems research.

Industry & Government

Partner on applied research

Work with us on crashworthiness testing, simulation contracts, and safety standards development for aviation, defense, and space applications.

Discuss a partnership →

Academic Collaboration

Research exchange & joint projects

We welcome joint research proposals, student exchanges, and co-authorship across aerospace engineering, computational mechanics, and space systems.

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Graduate Research

Join the lab as a researcher

Prospective PhD and MS students with backgrounds in aerospace, mechanical engineering, or computational simulation are encouraged to apply.

Apply to the lab →