The effect of a 70゜ swept canard on the leading-edge vortices of a 70゜ swept delta wing during dynamic pitching AIAA-97-0613

The effect of a 70゜ swept canard on the leading-edge vortices of a 70゜ swept delta wing during dynamic pitching

AIAA-97-0613

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Material Type: 規格・テクニカルリポート類
Title: The effect of a 70゜ swept canard on the leading-edge vortices of a 70゜ swept delta wing during dynamic pitching
Author/Editor: Hayashibara, Shigeo
Myose, Roy Y
Miller, L. Scott
Publication Date: 1997
Publication Date (W3CDTF): 1997
Extent: 8 p
Alternative Title: Aerospace sciences meeting & exhibit. 35th. Reno, Nev. Jan. 1997
Report No.: テクニカルリポート番号 : AIAA-97-0613
Holding library: 国立国会図書館
Call No.: M-AIAA-97-0613
Data Provider (Database): 国立国会図書館 : 国立国会図書館蔵書
https://ndlsearch.ndl.go.jp
Bibliographic ID (NDL): 000005860405
http://id.ndl.go.jp/bib/000005860405
Bibliographic Record Category (NDL): 291