Response Surface Modeling Tolerance and Inference Error Risk Specifications: Proposed Industry Standards-Reference-Cited by-同舟云学术

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Response Surface Modeling Tolerance and Inference Error Risk Specifications: Proposed Industry Standards

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference
language:
Short-container-title:

Author:

DeLoach Richard¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2859

Reference13 articles.

1. Applications of modern experiment design to wind tunnel testing at NASA Langley Research Center

2. 2DeLoach,R."TailoringWindTunnelDataVolumeRequirementsThroughtheFormalDesignOfExperiments,"AIAA98-2884,20th AdvancedMeasurementandGroundTestingConference,Albuquerque,NewMexico, June1998.

3. 3DeLoach,R."ImprovedQualityinAerospaceTestingThroughtheModernDesignofExperiments(Invited),"AIAA2000-0825,38th AIAAAerospace SciencesMeetingand Exhibit,Reno,Nevada, January2000.

4. Putting Ten Pounds in a Five-Pound Sack: Configuration Testing with MDOE

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1. Nonlinear Unsteady Aerodynamic Modeling Using Wind-Tunnel and Computational Data;Journal of Aircraft;2017-03

2. Nonlinear Unsteady Aerodynamic Modeling Using Wind Tunnel and Computational Data - Invited;AIAA Atmospheric Flight Mechanics Conference;2016-01-01

3. Aircraft Wind Tunnel Characterization using Modern Design of Experiments;54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2013-04-05

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