XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils

Details 詳細情報について

• CRID

  1363951793211130624

• DOI

  10.1007/978-3-642-84010-4_1

• ISSN

  01765035

• Web Site

  http://link.springer.com/content/pdf/10.1007/978-3-642-84010-4_1.pdf

• Data Source

  • Crossref