Publication:
A second law approach to aircraft conceptual design

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Authors
Gleeson, David A.
Subjects
NA
Advisors
Newberry, Conrad F.
Date of Issue
1998-09
Date
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
With advancements in the fields of propulsion, aerodynamics, structures, materials and controls, the routine exploration of hypersonic, atmospheric flight has become a more feasible concept. Thus, there is a need for efficient and effective hypersonic configurations. Current studies in configuration efficiency and effectiveness seem to be concentrated in aircraft subsystem design, especially propulsion systems, rather than at the conceptual aircraft system design level. This thesis attempts to initiate the process of incorporating the Second Law of Thermodynamics into the conceptual aircraft design process. The methodology for this process involves the use of the thermodynamic variable exergy, also known as availability. The ultimate goal of the process introduced by this thesis is to be able to define an aircraft configuration design space based upon both the First and Second Laws of Thermodynamics.
Type
Thesis
Description
Series/Report No
Department
Aeronautical Engineering
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Funder
Format
xv, 58 p.;28 cm.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
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