Aerospace research through statistical engineering
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Authors
Silvestrini, Rachel T.
Parker, Peter A.
Subjects
Design of experiments
Face-centered cube
Repeat measures
Replication
Sample size
Face-centered cube
Repeat measures
Replication
Sample size
Advisors
Date of Issue
2012
Date
Publisher
Taylor & Francis
Language
Abstract
The application of statistical engineering as described here is applied to fundamental research I support of hypersonic air breathing propulsion. An aerospace experiment that took place in a wind tunnel is the application of interest. One goal of the project was to accurately model the relationship between specific input and output parameters in the hypersonic combustion process within a controlled environment. Response surface methodology (RSM) was applied in a nontraditional manner to develop the response surface as the final deliverable rather than a tool to optimize a product or process.
Type
Article
Description
The article of record as published may be found at: http://dx.doi.org/10.1080/08982112.2012.641146
Series/Report No
Department
Operations Research
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funding
Format
14 p.
Citation
Quality Engineering, v.24, 2012, pp. 292-305
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.