Explore: Slender Wings
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Source: The Open Library
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1Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
By Julio Chu
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Metadata:
- Title: ➤ Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Author: Julio Chu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Subjects and Themes:
- Subjects: ➤ Vortices - Pressure distribution - Wind tunnel tests - Subsonic speed - Slender wings - Reynolds number - Delta wings - Leading edges - Mach number
Edition Identifiers:
- The Open Library ID: OL15504600M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
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2Natural rolling responses of a delta wing in transonic and subsonic flows
By Margaret A. Menzies
“Natural rolling responses of a delta wing in transonic and subsonic flows” Metadata:
- Title: ➤ Natural rolling responses of a delta wing in transonic and subsonic flows
- Author: Margaret A. Menzies
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Aeronautics
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Reston, Va - [Springfield, Va
“Natural rolling responses of a delta wing in transonic and subsonic flows” Subjects and Themes:
- Subjects: ➤ Flow equations - Fluid dynamics - Rigid structures - Subsonic flow - Swept wings - Navier-Stokes equation - Slender wings - Delta wings - Transonic flow
Edition Identifiers:
- The Open Library ID: OL15508546M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Natural rolling responses of a delta wing in transonic and subsonic flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.