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Transonic flow field around the CF-18 wing at angle of attack 4.5 deg

From National Research Council Canada

Alternative titleTransonic flow field around the CF-18 wing at angle of attack 4.5°
DOIResolve DOI: https://doi.org/10.2514/6.2000-797
AuthorSearch for: 1; Search for: 1ORCID identifier: https://orcid.org/0009-0008-0777-7919; Search for: 1
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Article
Conference38th Aerospace Sciences Meeting and Exhibit, January 10-13, 2000, Reno, Nevada, United States
Publication date
PublisherAmerican Institute of Aeronautics and Astronautics
In
LanguageEnglish
Peer reviewedYes
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Record identifier0d1b4d20-e39c-42b8-8e65-4a94766e1bb5
Record created2025-11-26
Record modified2025-11-26
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