Coupled rolling and pitching oscillation effects on transonic shock-induced vortex-breakdown flow of a delta wing AIAA-96-0828

Coupled rolling and pitching oscillation effects on transonic shock-induced vortex-breakdown flow of a delta wing

AIAA-96-0828

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Material Type: 規格・テクニカルリポート類
Title: Coupled rolling and pitching oscillation effects on transonic shock-induced vortex-breakdown flow of a delta wing
Author/Editor: Kandil, Osama A
Menzies, Margaret A
Publication Date: 1996
Publication Date (W3CDTF): 1996
Extent: 10 p
Alternative Title: Aerospace sciences meeting & exhibit. 34th. Reno, Nev. Jan. 1996
Report No.: テクニカルリポート番号 : AIAA-96-0828
Holding library: 国立国会図書館
Call No.: M-AIAA-96-0828
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): 000005535143
http://id.ndl.go.jp/bib/000005535143
Bibliographic Record Category (NDL): 291