Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft
The objective of this study is to use Multidisciplinary Design Optimization (MDO) to investigate the use of truss-braced wing concepts in concert with other advanced technologies to obtain a significant improvement in the performance of transonic transport aircraft. The truss topology introduces sev...
Main Author: | Grasmeyer, Joel M. III |
---|---|
Other Authors: | Aerospace and Ocean Engineering |
Format: | Others |
Published: |
Virginia Tech
2014
|
Subjects: | |
Online Access: | http://hdl.handle.net/10919/36729 http://scholar.lib.vt.edu/theses/available/etd-4598-173228/ |
Similar Items
-
The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts
by: Ko, Yan-Yee Andy
Published: (2014) -
Structural Optimization and Design of a Strut-Braced Wing Aircraft
by: Naghshineh-Pour, Amir H.
Published: (2014) -
Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport
by: Gundlach, John Frederick
Published: (2014) -
Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft
by: Meadows, Nicholas Andrew
Published: (2014) -
Multidisciplinary Design Optimization of Low-Noise Transport Aircraft
by: Leifsson, Leifur Thor
Published: (2014)