Optimization and design of a morphing wing tip aircraft demonstrator for drag reduction at low speeds, Part II – Experimental validation using infra-red transition measurements during wind tunnel tests

From National Research Council Canada

Download
  1. (PDF, 1 MB)
DOIResolve DOI: https://doi.org/10.1016/j.cja.2016.12.018
AuthorSearch for: ; Search for: ; Search for: ; Search for: ; Search for: ; Search for: ; Search for: 1 ; Search for: 1 
Name affiliation
  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Journal titleChinese Journal of Aeronautics
ISSN1000-9361
Subjectdrag reduction; infra-red tests; morphing wing; optimization; wind tunnel test
Abstract
Publication date
PublisherScienceDirect
LanguageEnglish
Peer reviewedYes
NPARC number23001243
Export citationExport as RIS
Report a correctionReport a correction
Record identifierffa11266-d9f4-4762-9715-ae85ba0ed8af
Record created2017-01-11
Record modified2019-03-08
Date modified: