1. Development of the in Situ Load System for internal wind-tunnel balances;Commo;J. Aircraft,2015
2. Flight reynolds number testing of the orion launch abort vehicle in the NASA langley national transonic facility (invited);Chan,2011
3. Thermal and pressure characterization of a wind tunnel force balance using the single vector system;Lynn,2011
4. Novel online re-calibration method for multi-axis force/torque sensor of ITER welding/machining robot;Roozbahzni;IEEE Sens. J.,2013
5. A triaxial cutting force measurement utilizing an embedded transducer on a spindle rotating tool;Rizal,2015