Explore: Supersonics
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Source: The Open Library
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Search results from The Open Library
1Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5
By Peter F. Covell
“Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5” Metadata:
- Title: ➤ Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5
- Author: Peter F. Covell
- Language: English
- Number of Pages: Median: 173
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Supersonic - Cone - Conical forebody - Supersonic Aerodynamics - Supersonics
Edition Identifiers:
- The Open Library ID: OL19244133M - OL15363711M - OL17106254M - OL18054341M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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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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2Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
By E. Carson Yates
“Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” Metadata:
- Title: ➤ Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
- Author: E. Carson Yates
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Inviscid flow - Viscous flow - Integral equations - Unsteady aerodynamics - Transonic flow - Computer aided design - Supersonics
Edition Identifiers:
- The Open Library ID: OL20650523M - OL17630478M - OL16131061M - OL18246750M
- Online Computer Library Center (OCLC) ID: 25058132
Access and General Info:
- First Year Published: 1990
- 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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3Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
By A. B. Blair
“Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Metadata:
- Title: ➤ Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
- Author: A. B. Blair
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service - Langley Research Center
- Publish Date: 1986
- Publish Location: ➤ Hampton, Va - Washington, D.C - Springfield, Va
“Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Cavitation flow - Cavities (Airplanes) - Cavity flow - Flat plates - Flow distribution - Flow visualization - Supersonic Aerodynamics - Supersonics - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19986377M - OL18290608M - OL17727208M
Access and General Info:
- First Year Published: 1986
- 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:
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4Study of lee-side flows over conically cambered delta wings at supersonic speeds
By Richard M. Wood
“Study of lee-side flows over conically cambered delta wings at supersonic speeds” Metadata:
- Title: ➤ Study of lee-side flows over conically cambered delta wings at supersonic speeds
- Author: Richard M. Wood
- Language: English
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Study of lee-side flows over conically cambered delta wings at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Supersonic - Delta wing airplanes - Delta wings - Supersonic Aerodynamics - Supersonics
Edition Identifiers:
- The Open Library ID: OL19044550M - OL15274155M - OL18028620M
Access and General Info:
- First Year Published: 1987
- 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 Study of lee-side flows over conically cambered delta wings at supersonic speeds at online marketplaces:
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- Ebay: New & used books.