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Investigation on the effect of canard angle of attack and position on the pressure distribution of a wing in a delta canard-wing-body configuration with PSW Software Pocket
Department of Aerospace, Sharif University of Technology, Tehran.
2009 (English)Conference paper, Oral presentation only (Refereed)
Place, publisher, year, edition, pages
2009.
Identifiers
URN: urn:nbn:se:ltu:diva-31704Local ID: 5f595e53-0720-4550-b52e-7e0ac5d941baOAI: oai:DiVA.org:ltu-31704DiVA, id: diva2:1004938
Conference
Annual International Conference of Iranian Aerospace Society : 17/02/2009 - 19/02/2009
Note
Upprättat; 2009; 20140123 (kavami)Available from: 2016-09-30 Created: 2016-09-30 Last updated: 2017-11-25Bibliographically approved

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Amiri, Kaveh

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CiteExportLink to record
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Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
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