Explore: Mixing Length Flow Theory
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Source: The Open Library
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1Mixing of an airblast-atomized fuel spray injected into a crossflow of air
By May Y. Leong
“Mixing of an airblast-atomized fuel spray injected into a crossflow of air” Metadata:
- Title: ➤ Mixing of an airblast-atomized fuel spray injected into a crossflow of air
- Author: May Y. Leong
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2000
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“Mixing of an airblast-atomized fuel spray injected into a crossflow of air” Subjects and Themes:
- Subjects: ➤ Fuel sprays - Mixing length flow theory - Gas injection - Air flow - Cross flow - Atomizing
Edition Identifiers:
- The Open Library ID: OL18171250M - OL17718829M - OL17607412M
- Online Computer Library Center (OCLC) ID: 50118145
Access and General Info:
- First Year Published: 2000
- 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.
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2A modified mixing length turbulence model for zero and adverse pressure gradients
By J. M. Conley and B. P. Leonard
“A modified mixing length turbulence model for zero and adverse pressure gradients” Metadata:
- Title: ➤ A modified mixing length turbulence model for zero and adverse pressure gradients
- Authors: J. M. ConleyB. P. Leonard
- Language: English
- Publisher: ➤ [National Technical Information Service, distributor] - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, VA] - [Springfield, Va
“A modified mixing length turbulence model for zero and adverse pressure gradients” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Turbulent boundary layer - Mixing length flow theory - Pressure gradients - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15408463M - OL18078587M
- Online Computer Library Center (OCLC) ID: 32660592
Author's Alternative Names:
"J.M Conley"Access and General Info:
- First Year Published: 1994
- 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 A modified mixing length turbulence model for zero and adverse pressure gradients at online marketplaces:
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3Supersonic coaxial jet noise predictions
By Milo D. Dahl
“Supersonic coaxial jet noise predictions” Metadata:
- Title: ➤ Supersonic coaxial jet noise predictions
- Author: Milo D. Dahl
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Supersonic coaxial jet noise predictions” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Mixing length flow theory - Turbulence models - Supersonic jet flow - Coaxial flow - Noise prediction (Aircraft) - Noise reduction - Aeroacoustics - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15413486M - OL17791557M
- Online Computer Library Center (OCLC) ID: 33441989
Access and General Info:
- First Year Published: 1995
- 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 Supersonic coaxial jet noise predictions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.