عنوان
پدید آورنده
موضوع
رده
کتابخانه
محل استقرار
NATIONAL BIBLIOGRAPHY NUMBER
Number
TL50816
LANGUAGE OF THE ITEM
.Language of Text, Soundtrack etc
انگلیسی
TITLE AND STATEMENT OF RESPONSIBILITY
Title Proper
Design of Advanced Skin Structure using Lattice for Camber Morphing Wing
General Material Designation
[Thesis]
First Statement of Responsibility
Alsaidi, Bashir Fawaz
Subsequent Statement of Responsibility
Joe, Woong Yeol
.PUBLICATION, DISTRIBUTION, ETC
Name of Publisher, Distributor, etc.
Tennessee State University
Date of Publication, Distribution, etc.
2019
GENERAL NOTES
Text of Note
158 p.
DISSERTATION (THESIS) NOTE
Dissertation or thesis details and type of degree
Ph.D.
Body granting the degree
Tennessee State University
Text preceding or following the note
2019
SUMMARY OR ABSTRACT
Text of Note
When any morphing wing structures and controls are considered, an important parameter is often overlooked, which is the skin for the wing. Conventional fixed wings only require a certain thickness of skin material/structure to endure aerodynamic loading in general. However, the nature of morphing wings that constantly change and adjust wing shapes to optimize the flight performance makes the skin design much more complicated and challenging. When the wing morphs, the skin should comply with the altered geometry while maintaining its stiffness for aerodynamic loadings in various flight modes. Advantages of flexible skins include their large deformation capability and low elastic modulus. However, many works in the design of skins for morphing wings, which typically use smart materials, consider only geometric or static deformations but not dynamic ones. A simple geometry-structured material for skin is not very compliant for multi-dimensional morphing motions such as camber change and twisting, limited in meeting various aerodynamic and structural loadings and stresses, and expensive to establish design process for customized skins for morphing wings. The main theme of this proposal is to design advanced skin structures for camber morphing wing aircraft. Thus, this study focuses on skin design process and procedure for Variable Camber Compliant Wings (VCCW) thorough modeling, stress/strain analysis, and experiments of solid and lattice structures.
UNCONTROLLED SUBJECT TERMS
Subject Term
Engineering
Subject Term
Materials science
Subject Term
Mechanical engineering
PERSONAL NAME - PRIMARY RESPONSIBILITY
Alsaidi, Bashir Fawaz
PERSONAL NAME - SECONDARY RESPONSIBILITY
Joe, Woong Yeol
CORPORATE BODY NAME - SECONDARY RESPONSIBILITY
Tennessee State University
ELECTRONIC LOCATION AND ACCESS
Electronic name
مطالعه متن کتاب p
[Thesis]
276903
a
Y
