Prediction of flutter and inlet distortion driven response of a transonic fan rotor using phase-lagged boundary conditons ASME-2001-GT-272

Prediction of flutter and inlet distortion driven response of a transonic fan rotor using phase-lagged boundary conditons

ASME-2001-GT-272

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Material Type: 規格・テクニカルリポート類
Title: Prediction of flutter and inlet distortion driven response of a transonic fan rotor using phase-lagged boundary conditons
Author/Editor: Li, H. D
He, L
Publication Date: 2001
Publication Date (W3CDTF): 2001
Extent: 9 p
Alternative Title: International gas turbine & aeroengine congress & exhibition. New Orleans, La. Jun. 2001
Report No.: テクニカルリポート番号 : ASME-2001-GT-272
Holding library: 国立国会図書館
Call No.: M-ASME-2001-GT-272
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): 000006094679
http://id.ndl.go.jp/bib/000006094679
Bibliographic Record Category (NDL): 291