This test aircraft, hence the ACTE control surfaces, was flown at 0.85 Mach, maximum altitude of 40,000 ft. and were subjected to 2G maneuvers and a maximum dynamic pressure of 384 psf.

“The (Flexfoil) technology has performed flawlessly… Data taken from the flight demonstration supports the potential for reducing fuel burn by 5 to 10 percent for a clean sheet design of advanced subsonic commercial transport." ” - Dr. Fay Collier, Director - Environmentally Responsible Aviation, NASA

“The FlexFoil control surface technology will soon be credited with revolutionizing the aircraft industry by dramatically improving fuel efficiency and enabling quiet aircraft operation”. - Peter Flick, Air Force Research Lab


Professor Sridhar Kota founded FlexSys in 2001 to engineer and flight test his patented shape-changing aircraft wings in collaboration with the Air Force Research Laboratory and NASA. The key to success is our unique approach to mechanical design by exploiting material elasticity – called distributed compliant design. Today, companies of all sizes across industries contract FlexSys to pursue innovation through the application of Compliant Design to create sophisticated mechanical motions without joints. Whether it is a clean-sheet design, or rethinking a current product, FlexSys has a creative team of engineers and a full suite of hardware and software tools that can help.

SridharKota Home Page

Contact Us today for your innovation of tomorrow.


“The most incredible mechanical and aeronautical engineering idea that I have seen since I graduated 60 years ago! Perhaps in all the history of flight.” - Charles S. Hutchins, Father of Computer-Aided Manufacturing (CAM).


Engineering with Elasticity


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Recipient 2015 Tibbetts Award

Recipient Tibbetts Award

Recipient National Science Foundation SBIR Grants

Recipient National Science Foundation SBIR Grants

Recipient Air Force SBIR Grants

Recipient Air Force SBIR Grants

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