Results 111 to 120 of about 11,252 (231)

Structural dynamics branch research and accomplishments to FY 1992 [PDF]

open access: yes
This publication contains a collection of fiscal year 1992 research highlights from the Structural Dynamics Branch at NASA LeRC. Highlights from the branch's major work areas--Aeroelasticity, Vibration Control, Dynamic Systems, and Computational ...
Lawrence, Charles
core   +1 more source

Aerolastic tailoring and integrated wing design [PDF]

open access: yes
Much has been learned from the TSO optimization code over the years in determining aeroelastic tailoring's place in the integrated design process. Indeed, it has become apparent that aeroelastic tailoring is and should be deeply embedded in design ...
Bohlmann, Jon, Love, Mike H.
core   +1 more source

Whirl Flutter and the Development of the NASA X-57 Maxwell [PDF]

open access: yes
The X-57 Maxwell is NASAs all-electric demonstration vehicle. The primary demonstration objective of this flight test program is to show a factor of five reduction in energy consumption.
Heeg, Jennifer   +5 more
core   +1 more source

Status and Perspectives of Commercial Aircraft Morphing. [PDF]

open access: yesBiomimetics (Basel), 2022
Giuliani M   +4 more
europepmc   +1 more source

Computational aeroelasticity challenges and resources [PDF]

open access: yes
In the past decade, there has been much activity in the development of computational methods for the analysis of unsteady transonic aerodynamics about airfoils and wings.
Edwards, John W.
core   +1 more source

Design and analysis issues of integrated control systems for high-speed civil transports [PDF]

open access: yes
A study was conducted to identify, rank, and define development plans for the critical guidance and control design and analysis issues as related to economically viable and environmentally acceptable high-speed civil transport. The issues were identified
Dykman, John R.   +4 more
core   +1 more source

Determining structural performance [PDF]

open access: yes
An overview of the methods and concepts developed to enhance and predict structural dynamic characteristics of advanced aeropropulsion systems is presented. Aeroelasticity, vibration control, dynamic systems, and computational structural methods are four
Brown, Gerald   +9 more
core   +1 more source

Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model [PDF]

open access: yes
The CAP-TSD (Computational Aeroelasticity Program - Transonic Small Disturbance) code, developed at the NASA - Langley Research Center, is applied to the Active Flexible Wing (AFW) wind tunnel model for prediction of the model's transonic aeroelastic ...
Bennett, Robert M., Silva, Walter A.
core   +1 more source

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