Overview of the DARPA Smart Wing Project. The recently completed DARPA/AFRL/NASA Smart Wing program, performed by a team led by Northrop Grumman Corporation. NGC), addressed the development and demonstration of smart materials based concepts to improve the aerodynamic. This paper presents an overview of the program. The program was divided into two phases.
DARPA/AFRL/NASA Smart Wing Second Wind Tunnel Test Results. SMART WING TEST 2 OVERVIEW. “Overview of DARPA / AFRL / NASA Smart Wing Program”. Under Phase 1 (January 1. February 1. NGC- led team developed. Abstract. The recently completed DARPA/AFRL/NASA Smart Wing program, performed by a team led by Northrop Grumman Corporation (NGC. The DARPA/AFRL/NASA Smart Wing program. under the DARPA Smart Materials and. and Ephrahim Garcia 'Overview of the DARPA/AFRL/NASA Smart Wing Phase II. An important limitation of the. Phase 1 effort, the low bandwidth achievable in Shape Memory Alloy (SMA)- based actuation, was addressed in. Phase 2 (January 1. November 2. 00. 1). Under Phase 2, a 3. NGC Uninhabited Combat Air Vehicle (UCAV) design was developed. For the Phase 2 first wind tunnel test. March 2. 00. 0, SMA- actuated, hingeless, smoothly contoured, flexible leading and trailing edge control. This test provided baseline steady- state data at Mach numbers ranging. The test also demonstrated the benefits of the smart leading edge control surface to compensate. The second test, performed in May 2. Spanwise and chordwise shape control was demonstrated for the smart trailing edge. Performance improvements in terms of increased rolling. The work performed.
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September 2016
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