Results 121 to 130 of about 2,602 (169)

Aeroelastic Tailoring Study in Aircraft Design

, 1985
T. Ugai, H. Kikikawa, J. Takaki, M. Sunakawa, Y. Hirano   +4 more
openaire   +2 more sources

Robust Aeroelastic Optimisation of Composite Plate Wings Subject to Ply Orientation Uncertainty [PDF]

, 2015
Cooper, Jonathan, Sartor, Pia, Scarth, Carl, Silva, Gustavo H C, Weaver, Paul   +4 more
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A novel dynamic aeroelastic framework for aeroelastic tailoring and structural optimisation

Composite Structures, 2016
Driven by a need to improve the efficiency of aircraft and reduce the fuel consumption, composite materials are applied extensively in the design of aircraft. A dynamic aeroelastic framework for the conceptual design of a generic composite wing structure is presented. The wing is discretised in several spanwise sections, where each section has a number
Noud Werter, Roeland De Breuker
exaly   +4 more sources

Aeroelastic Tailoring and Active Aeroelastic Wing Impact on a Lambda Wing Configuration

Journal of Aircraft, 2017
Two aeroelastic design approaches are applied to a supersonic lambda wing configuration with the goal of improving the wing’s aeroelastic performance. Aeroelastic tailoring and active aeroelastic wing technologies are investigated in a sequential manner to quantify their benefits. Industry-standard tools are used to perform these design studies. First,
Edward J Alyanak
exaly   +2 more sources

Aeroelastically Tailored Propellers

SAE Technical Paper Series, 1977
<div class="htmlview paragraph">An analytical investigation into the possible improvement of aircraft propeller performance that may be obtained by employing high strength filamentary composite materials to modify the elastic characteristics of the blades was conducted.
W. J. Dwyer, J. B. Rogers
openaire   +1 more source

Robust design for aeroelastically tailored/active aeroelastic wing

7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 1998
Presented at the 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, St. Louis, MO, September 2-4, 1998.
P. Zink, Dimitri Mavris, Michael Love, Mordechay Karpel   +3 more
openaire   +1 more source

Aeroelastic Tailoring of Composite Structures

Journal of Aircraft, 1999
A wing-design optimization study is conducted on a composite wing. The objective is to evaluate the effect of the compositelayup orientation on theoptimized weight while satisfying constraints on strength, roll-reversalvelocity, and e utter velocity. The wing optimization studies are presented with the composite layups oriented at 5-deg increments up ...
F. E. Eastep, V. A. Tischler, V. B. Venkayya, N. S. Khot   +3 more
openaire   +1 more source

Aeroelastic Tailoring for Gust-Energy Extraction

Journal of Aerospace Engineering, 2020
AbstractFor small fixed-wing aircraft, passive forms of extracting energy from the atmosphere have been shown to have positive improvements on their flight performance.
Michael Melville, Götz Bramesfeld, Amir Kolaei, Hekmat Alighanbari   +3 more
openaire   +1 more source