Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By John W. Edwards
"Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method" is published by National Aeronautics and Space Administration, Langley Research Center in 1996 - Hampton, Va and the language of the book is English.
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Metadata:
- Title: ➤ Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Author: John W. Edwards
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow equations - Unsteady flow - Separated flow - Transonic flow - Transonic flutter - Mach number - Unsteady aerodynamics
Edition Specifications:
- Format: Microform
- Pagination: 1 v.
Edition Identifiers:
- The Open Library ID: OL17838507M - OL11602496W
- Online Computer Library Center (OCLC) ID: 40173648
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