Boundary-layer displacement and leading-edge bluntness effects on attached and separated laminar boundary layers in a compression corner. II - Experimental study

• MICHAEL S. HOLDEN

  Cornell Aeronautical Laboratory, Inc., Buffalo, N. Y.

収録刊行物

• AIAA Journal

  AIAA Journal 9 (1), 84-93, 1971-01

  American Institute of Aeronautics and Astronautics (AIAA)

キーワード

• Aerospace Engineering

詳細情報

• CRID: 1360292621568677120
• NII論文ID: 30037748622
• DOI: 10.2514/3.6127
• ISSN: 1533385X
• ISSN: 00011452
• ISSN: http://id.crossref.org/issn/00011452
• Web Site: http://arc.aiaa.org/doi/pdf/10.2514/3.6127
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