Purdue University
Researchers at Purdue University are experimenting with electronic systems capable of morphing to meet the requirements of changing hypersonic operating conditions.

Stable Structures Morph with Hypersonic Conditions

April 12, 2024
Andres Arrieta and his research group at Purdue University are experimenting with electronic systems capable of morphing to meet the requirements of changing hypersonic operating conditions.

Electronic systems operated within hypersonic vehicles, such as missiles, must withstand rapidly changing operating environments, placing tremendous stress on many components. To better prepare electrical and mechanical components for these harsh operating environments, researchers at Purdue University are experimenting with morphing systems capable of adapting to changing environments. They are researching the materials and structures required for successful and reliable performance under stressful operating conditions within hypersonic missiles.

At Purdue (West Lafayette, IN), Andres Arrieta, associate professor of mechanical engineering, and Rodney Trice, professor of materials engineering, are designing aircraft systems with multistable structures (see figure). They are exploring combinations of materials and physical structures capable of adapting to changing operating conditions. They are also considering the requirements of different applications, such as the need for lighter-weight materials and structures for achieving longer flight times in aircraft and missile systems. 

The structures they are seeking can morph in shape and in weight in response to external forces. These structures function through a combination of mechanical and material interventions that not only make morphing hypersonic systems possible but may also reduce weight and complexity. The technology is based on data from advanced sensors and structures programmed to respond to changes according to localized sensors. According to Arrieta, “Current mechanisms that help aircraft maneuver, like the aileron or tail, create noise and drag. These mechanisms are also chains of various parts, and each of these parts is joined by a joint. The more parts and joints you have, the more complex your system becomes.” As the solution, he explains: “So if we have a structure that is just one big part but is also capable of deforming, then there is potential to reduce not only complexity but also failure, maintenance costs and weight — which is the most important consideration in aviation.” The Purdue researchers are attempting to develop surfaces that can take on a variety of shapes for optimum performance over a range of aircraft speeds.

Sponsored Recommendations

Guide to VNA Automation in MATLAB Using the TCP Interface

April 19, 2024
In this guide, advantages of using MATLAB with TCP interface is explored. The how-to is also covered for setting up automation language using a CMT VNA.

In-Circuit Antenna Verification

April 19, 2024
In this video, Brian Walker, Senior RF Design Engineer at Copper Mountain Technologies, shows how there can be significant variation of the performance of a PCB-mounted antenna...

UHF to mmWave Cavity Filter Solutions

April 12, 2024
Cavity filters achieve much higher Q, steeper rejection skirts, and higher power handling than other filter technologies, such as ceramic resonator filters, and are utilized where...

Wideband MMIC Variable Gain Amplifier

April 12, 2024
The PVGA-273+ low noise, variable gain MMIC amplifier features an NF of 2.6 dB, 13.9 dB gain, +15 dBm P1dB, and +29 dBm OIP3. This VGA affords a gain control range of 30 dB with...