Design, fabrication, and testing of scaled wind tunnel model for the Smart Wing Phase 2 program

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 4332, Issue , 2001, Pages 399-406

  Martin, C A ^a   Scherer, L B ^a   Flanagan, J S ^a   Carpenter, B F ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; INTELLIGENT MATERIALS; PRESSURE EFFECTS; SHAPE MEMORY EFFECT; SURFACES; TRANSONIC AERODYNAMICS; WINGS;

EDGE CONTROL SURFACES; TRANSONIC MACH NUMBERS;

WIND TUNNELS;

EID: 0034844880     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.429681     Document Type: Conference Paper

References (5)

1. Overview of the DARPA/AFRL/NASA "Smart Wing" program
2. Design and fabrication of Smart Wing model and SMA control surfaces
3. Aerodynamic and aeroelastic characteristics of the DARPA Smart Wing Phase II wind tunnel model
4. Development of high-rate, large deflection, hingeless trailing edge control surface for the Smart Wing wind tunnel model