Results 91 to 100 of about 3,197 (203)

Flow Control around the UAS-S45 Pitching Airfoil Using a Dynamically Morphing Leading Edge (DMLE): A Numerical Study. [PDF]

Biomimetics (Basel), 2023
Bashir M, Zonzini N, Botez RM, Ceruti A, Wong T.   +4 more
europepmc   +1 more source

Lifting-Line Predictions for the Ideal Twist Effectiveness of Spanwise Continuous and Discrete Control Surfaces

Applied Sciences
Modern materials and manufacturing technologies have allowed the construction of morphing wings that are able to continuously vary certain airfoil parameters such as twist, camber, or control surface deflection as a function of span. This work presents a
Zachary S. Montgomery, Douglas F. Hunsaker, James J. Joo   +2 more
doaj   +1 more source

Enhanced Range and Endurance Evaluation of a Camber Morphing Wing Aircraft. [PDF]

Biomimetics (Basel), 2023
Jo BW, Majid T.
europepmc   +1 more source

The use of actuated flexible plates for adaptive shock control bumps [PDF]

, 2015
Ashill P., Klemens N., Lee D., Rhodes O., Sommerer A., Th., L.   +4 more
core   +1 more source

A Numerical Study on Smart Material Selection for Flapped and Twisted Morphing Wing Configurations

Journal of Aerospace Technology and Management, 2014
The developments of innovative adaptive structures on Unmanned Aerial Vehicles (UAVs), such as morphing wings, can potentially reduce system complexities by eliminating control surfaces and their auxiliary equipment. This technology has the potential of
Maurício Vicente Donadon, Lorenzo Iannucci   +1 more
doaj  

Computational Investigation on the Effects of Two-Way Wing Morphing Strategy in the Critical Mach Number

Journal of Aerospace Technology and Management, 2018
The elasto-flexible wing morphing is an advanced methodology to achieve higher lift-to-drag (L/D) ratio for the subsonic wing configurations at the given flow conditions.
Bruce Ralphin Rose John, Baby Usha Sivathanu, Bibal Benifa John Vijaya   +2 more
doaj  

Rapid Assessment of Aircraft Structural Topologies for Multidisciplinary Optimization and Weight Estimation [PDF]

Algorithms for rapid generation of moderate-fidelity structural finite element models of air vehicle structures to allow more accurate weight estimation earlier in the vehicle design process have been developed.
Samareh, Jamshid A., Sensmeier, mark D., Stewart, Bret A.   +2 more
core   +1 more source

Manufacturing and Preliminary Testing of Nano-Filled Elastomeric Film Cover for Morphing Airfoil. [PDF]

Sensors (Basel)
Ciminello M, Piscitelli F, Volponi R, Ameduri S.   +3 more
europepmc   +1 more source

Research on Design and Control Method of Flexible Wing Ribs with Chordwise Variable Camber. [PDF]

Biomimetics (Basel)
Tao X, Bin L.
europepmc   +1 more source

Research on aerodynamic characteristics and control method of rigid-flexible variable camber wing. [PDF]

Sci Rep
Xin T, Li B.
europepmc   +1 more source