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Multidisciplinary Reference Solutions for Performance-Optimized Aircraft Wings with Tailored Aerodynamic Load Distributions.

Record Type:	Language materials, manuscript : Monograph/item
Title/Author:	Multidisciplinary Reference Solutions for Performance-Optimized Aircraft Wings with Tailored Aerodynamic Load Distributions./
Author:	Taylor, Jeffrey D.
Description:	1 online resource (514 pages)
Notes:	Source: Dissertations Abstracts International, Volume: 84-03, Section: B.
Contained By:	Dissertations Abstracts International84-03B.
Subject:	Mechanical engineering. -
Online resource:	click for full text (PQDT)
ISBN:	9798351453026

Multidisciplinary Reference Solutions for Performance-Optimized Aircraft Wings with Tailored Aerodynamic Load Distributions.
Taylor, Jeffrey D.

Multidisciplinary Reference Solutions for Performance-Optimized Aircraft Wings with Tailored Aerodynamic Load Distributions. - 1 online resource (514 pages)

Source: Dissertations Abstracts International, Volume: 84-03, Section: B.

Thesis (Ph.D.)--Utah State University, 2022.

Includes bibliographical references

Morphing wings, or wings that can change shape during flight, have the potential to substantially reduce the amount of fuel consumed by an aircraft over the course of its flight. However, the extent to which these wings can reduce fuel consumption depends on the design of the wing, including its aerodynamic efficiency and its structural layout, and how the aircraft flies, including its flight altitude and speed. Correctly predicting how these design and operational characteristics interact is critical to predicting how wing morphing may affect aircraft fuel consumption. Many computer prediction tools exist that include the effects of these interactions, but extracting the information needed to understand how the interactions work from most of these tools is very difficult. In this dissertation, some simplified models are presented that more directly reveal key information about the interplay between aerodynamics, structures, control, and the flight trajectory in the design of morphing wings. This information is used to characterize the impacts of wing morphing on aircraft efficiency.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024

Mode of access: World Wide Web

ISBN: 9798351453026Subjects--Topical Terms:

557493
Mechanical engineering.
Subjects--Index Terms:

AerodynamicsIndex Terms--Genre/Form:

554714
Electronic books.

Multidisciplinary Reference Solutions for Performance-Optimized Aircraft Wings with Tailored Aerodynamic Load Distributions.
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500 $a Advisor: Hunsaker, Douglas F.
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520 $a Morphing wings, or wings that can change shape during flight, have the potential to substantially reduce the amount of fuel consumed by an aircraft over the course of its flight. However, the extent to which these wings can reduce fuel consumption depends on the design of the wing, including its aerodynamic efficiency and its structural layout, and how the aircraft flies, including its flight altitude and speed. Correctly predicting how these design and operational characteristics interact is critical to predicting how wing morphing may affect aircraft fuel consumption. Many computer prediction tools exist that include the effects of these interactions, but extracting the information needed to understand how the interactions work from most of these tools is very difficult. In this dissertation, some simplified models are presented that more directly reveal key information about the interplay between aerodynamics, structures, control, and the flight trajectory in the design of morphing wings. This information is used to characterize the impacts of wing morphing on aircraft efficiency.
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653 $a Aerostructural optimization
653 $a Multidisciplinary design optimization
653 $a Trajectory optimization
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