Results 91 to 100 of about 1,956 (155)
Ground Strength Test Technique of Variable-Camber Wing Leading Edge
BiomimeticsMorphing wing technology is crucial for enhancing the flight performance of aircraft. To address the monitoring challenges of full-scale variable-camber leading edges under flight conditions, this study introduces a ground-based strength testing ...
Shanshan Li +3 more
doaj +1 more source
Distributed-Flap Layout Trade Study on a Highly Flexible Common Research Model [PDF]
The results of a layout trade study of a full-span, trailing-edge flap system for the NASACommon Research Model (CRM) are presented. Previously developed analysis and design tools areused to determine the potential performance benefits of several flap ...
Aftosmis, Michael J. +3 more
core +1 more source
Wing Shaping and Gust Load Controls of Flexible Aircraft: An LPV Approach [PDF]
In the proposed paper, the optimum wing shape of a highly flexible aircraft under varying flight conditions will be controlled by a linear parameter-varying approach.
Hammerton, Jared R. +3 more
core +1 more source
Self-Latching Piezocomposite Actuator [PDF]
A self-latching piezocomposite actuator includes a plurality of shape memory ceramic fibers. The actuator can be latched by applying an electrical field to the shape memory ceramic fibers.
Bryant, Robert G. +2 more
core +1 more source
Particle Image Velocimetry near Interfaces: A Moving Future [PDF]
, 2012 Theunissen, Raf
core +2 more sources
Computational Analysis of the Aerodynamics of Camber Morphing
AIAA Aviation 2019 Forum, 2019 Huntley, Sam +2 more
openaire +2 more sources
Experimental Investigation of a Morphing Nacelle Ducted Fan [PDF]
The application of Circulation Control to the nacelle of a shrouded fan is proposed as a means to enhance off-design performance of the shrouded fan. Typically, a fixed geometry shroud is efficient at a single operating condition.
Kondor, Shayne A., Moore, Mark
core +1 more source
Modeling of Tunable Elastic Ultralight Aircraft [PDF]
Aircraft weight is one of the most critical factors in the design and operation of modern vehicles. The ability to integrate ultra-light materials into the primary load bearing structures has the potential to reduce aircraft weight significantly ...
Cheung, Kenneth C. +4 more
core +1 more source
Aeroelastic Tailoring of Transport Aircraft Wings: State-of-the-Art and Potential Enabling Technologies [PDF]
This paper provides a brief overview of the state-of-the-art for aeroelastic tailoring of subsonic transport aircraft and offers additional resources on related research efforts. Emphasis is placed on aircraft having straight or aft swept wings.
Jutte, Christine, Stanford, Bret K.
core +1 more source